Kayhan Space Satcat

Watchlists

Notifications
No new unread notifications...

APEX ARIES 1, 59129

Orbit data source: Space-Track

APEX ARIES 1, 59129 is a payload satellite owned by Apex (US) in SSO that was launched on Mon, 04 Mar 2024 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

Loading next visibility...

Iframe embed code

<iframe src="https://www.satcat.com/sats-embedded/59129?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/59129?theme=dark&initialShowStats=false

Optional Secondary NORAD IDs

Max 10 NORAD IDs; Separated by commas

Initial load time (optional)

ISO8601 Format

TLE date request (optional)

ISO8601 Format

Identifier

59129, 2024-043AH

Orbit

SSO

Country

US

Related business

Apex Space (US)

Manufacturer

Apex

Mission

Operational Commercial Technology

Bus & Motor

ARIES, Unknown motor

Mass

200 kg wet, 200 kg dry

Launch date (UTC)

2024-03-04 (2 years ago)

Launch vehicle

FALCON 9

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Box + 2 Pan, 1.8 m

Radar Cross Section

1.983 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago

0 APEX ARIES 1
1 59129U 24043AH  26186.40570472  .00037706  00000-0  52718-3 0  9990
2 59129  97.5498 337.6619 0006278 133.3144 226.8635 15.56729478130759

Epoch: 2026-07-05T09:44Z

TLE epoch observation values (Epoch: 2026-07-05T09:44:12.887Z)

Latitude

-0.00004°

Longitude

-91.7973°

Altitude

403.176 km

Speed

7.667 km/s

True Right ascension

22h 30m 38s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

Unknown

Longitude

Unknown

Altitude

Unknown

Speed

Unknown

Apparent Right ascension

Unknown

Apparent Declination

Unknown

Sunlit

N/A

Visualization observer readout

Local Sidereal Time

23:25:46

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

398.305 km

Perigee altitude

389.802 km

Semi-major axis

6,772.19 km

Eccentricity

0.00063

Inclination

97.5498°

RAAN

337.6619°

Arg. of periapsis

133.3144°

True anomaly

226.81103°

Mean anomaly

226.8635°

Eccentric anomaly

226.83726°

Mean motion

3.89448 °/min

Orbital period

92.44 mins

BSTAR

0.00052718

Loading maneuver chart data...

Computing Atmospheric mass density...

Loading historical data...

Loading historical data...

Loading historical data...

Loading historical data...

Loading historical data...

Loading historical data...

Loading historical data...

Other satellites on launch #43 in the year 2024 (2024-03-04 UTC)

LACE-2, 59119 (Decayed)

PE2_FLT2 (TYVAK-0262), 59104

VSP RF C1, 59136

OBJECT R, 59113 (Decayed)

LACE-1, 59118 (Decayed)

LEMUR 2 FELDHUS, 59116 (Decayed)

OBJECT P, 59111 (Decayed)

SONATE-2, 59112

JACKAL-01, 59127

LYNK TOWER 6, 59123

Did you know?

You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.

Click here to try in Sandbox

APEX ARIES 1 Visibility forecast

Loading observer location...
Set Observer location

Span	Click to sort rows by Start time (UTC) header in descending order	Start Az.	Max El. time (UTC)	Max El. Az.	Max El.	End time (UTC)	End Az.
5 mins	2026-07-06 23:18:23.471Z	358.656° N	2026-07-06 23:21:23.471Z	277.731° WNW	34.55°	2026-07-06 23:23:23.471Z	217.663° SW

Items per page:

1–1 of 1 items

of 1 page

Co-orbital & Co-planar RSOs

Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions

Please sign-in to view Co-orbital & Co-planar RSOs.

Click to sort rows by RSO header in ascending order	Click to sort rows by Country header in ascending order	Click to sort rows by Type header in ascending order	Click to sort rows by Inclination Δ header in ascending order	Click to sort rows by RAAN Δ header in ascending order	Click to sort rows by Coplanar Angle header in ascending order	Click to sort rows by SMA Δ header in ascending order	Click to sort rows by Orbital period header in ascending order	Click to sort rows by <5km Md TCA header in descending order

CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings

Authenticating...

Click to sort rows by Secondary header in ascending order	Click to sort rows by Secondary name header in ascending order	Click to sort rows by Country header in ascending order	Click to sort rows by Owner header in ascending order	Click to sort rows by Obj. Type header in ascending order	Click to sort rows by Miss dist. header in ascending order	Click to sort rows by Rel. speed header in ascending order	Click to sort rows by Apr. angle header in ascending order	Click to sort rows by TCA header in descending order

Check out APEX ARIES 1, 59129 on other resources

View APEX ARIES 1, 59129 on NASA - NSSDCA Website

View APEX ARIES 1, 59129 on Heavens-Above

View APEX ARIES 1, 59129 on Keep Track

View APEX ARIES 1, 59129 on Celestrak

View APEX ARIES 1, 59129 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

Documentation

Go to standalone docs website

Showing up to 5 results

|