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.
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59129 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Apex
Mission
Operational Commercial Technology
Bus & Motor
ARIES, Unknown motor
Mass
200 kg wet, 200 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
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 & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 APEX ARIES 1
1 59129U 24043AH 26058.93344977 .00032055 00000-0 57493-3 0 9992
2 59129 97.5292 203.6208 0006402 229.2050 130.8646 15.49844503110963Epoch: 2026-02-27T22:24Z
TLE epoch observation values (Epoch: 2026-02-27T22:24:10.060Z)
Latitude
-0.00001°
Longitude
69.81607°
Altitude
423.156 km
Speed
7.656 km/s
True Right ascension
13h 34m 28s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
17:15:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
418.46 km
Perigee altitude
409.764 km
Semi-major axis
6,792.249 km
Eccentricity
0.00064
Inclination
97.5292°
RAAN
203.6208°
Arg. of periapsis
229.205°
True anomaly
130.92005°
Mean anomaly
130.8646°
Eccentric anomaly
130.89233°
Mean motion
3.87724 °/min
Orbital period
92.85 mins
BSTAR
0.00057493
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Other satellites on launch #43 in the year 2024 (2024-03-04 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.APEX ARIES 1 Visibility forecast
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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 | 2026-02-28 22:12:07.563Z | 23.681° NE | 2026-02-28 22:15:07.563Z | 114.17° SE | 37.691° | 2026-02-28 22:17:07.563Z | 172.778° S |
| 4 mins | 2026-03-01 10:11:07.563Z | 220.613° SW | 2026-03-01 10:12:07.563Z | 246.699° WSW | 23.283° | 2026-03-01 10:15:07.563Z | 320.329° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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 |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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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 |
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