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LEMUR 2 JOHNNYTRUONG, 59146

Orbit data source: Space-Track

LEMUR 2 JOHNNYTRUONG, 59146 is an American payload satellite 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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Iframe URL

https://www.satcat.com/sats-embedded/59146?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

59146, 2024-043BA

Orbit

SSO

Country

US

Related business

Spire Global (US)

Manufacturer

Spire/Glasgow

Mission

Operational Commercial Communications

Bus & Motor

CUBESAT 16U, Unknown motor

Mass

22 kg wet, 22 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 + 4 Pan, 1.4 m

Radar Cross Section

0.326 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 18 hours ago

TLE from 18 hours ago

0 LEMUR 2 JOHNNYTRUONG
1 59146U 24043BA  26235.37372283  .00043034  00000-0  42995-3 0  9997
2 59146  97.5415  31.5231 0002494 282.2357  77.8623 15.65501097138533

Epoch: 2026-08-23T08:58Z

TLE epoch observation values (Epoch: 2026-08-23T08:58:09.652Z)

Latitude

-0.00001°

Longitude

-74.68782°

Altitude

374.592 km

Speed

7.685 km/s

True Right ascension

02h 06m 05s

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

17:51:04

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

370.392 km

Perigee altitude

367.027 km

Semi-major axis

6,746.846 km

Eccentricity

0.00025

Inclination

97.5415°

RAAN

31.5231°

Arg. of periapsis

282.2357°

True anomaly

77.89024°

Mean anomaly

77.8623°

Eccentric anomaly

77.87627°

Mean motion

3.91644 °/min

Orbital period

91.92 mins

BSTAR

0.00042995

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

OBJECT AT, 59139 (Decayed)

VSP RF A1, 59135

APEX ARIES 1, 59129

IRIS-F1, 59110 (Decayed)

SENTRY, 59140 (Decayed)

METHANESAT, 59101

ICEYE-X38, 59100

ICEYE-X36, 59103

LYNK TOWER 6, 59123

ICEYE-X37, 59102

OBJECT AY, 59144 (Decayed)

PE2_FLT1 (TYVAK-0261), 59105

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

LEMUR 2 JOHNNYTRUONG 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.
4 mins	2026-08-24 23:52:57.627Z	335.531° NNW	2026-08-24 23:54:57.627Z	268.21° W	24.383°	2026-08-24 23:56:57.627Z	226.125° WSW

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Co-orbital & Co-planar RSOs

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

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

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Check out LEMUR 2 JOHNNYTRUONG, 59146 on other resources

View LEMUR 2 JOHNNYTRUONG, 59146 on NASA - NSSDCA Website

View LEMUR 2 JOHNNYTRUONG, 59146 on Heavens-Above

View LEMUR 2 JOHNNYTRUONG, 59146 on Keep Track

View LEMUR 2 JOHNNYTRUONG, 59146 on Celestrak

View LEMUR 2 JOHNNYTRUONG, 59146 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

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