LEMUR 2 AHMED-ASRAR, 60576
Orbit data source: Space-Track
LEMUR 2 AHMED-ASRAR, 60576 is an American payload satellite in SSO that was launched on Fri, 16 Aug 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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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Com/MetRO
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
7.6 kg wet, 7.6 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.5 m
Radar Cross Section
0.063 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 LEMUR 2 AHMED-ASRAR
1 60576U 24149DN 25340.83276873 .00017781 00000-0 11690-2 0 9995
2 60576 97.7167 59.6460 0001335 314.6653 45.4465 15.07646507 71538Epoch: 2025-12-06T19:59Z
TLE epoch observation values (Epoch: 2025-12-06T19:59:11.218Z)
Latitude
-0.00007°
Longitude
43.99442°
Altitude
545.81 km
Speed
7.59 km/s
True Right ascension
03h 58m 35s
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
13:33:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
541.313 km
Perigee altitude
539.466 km
Semi-major axis
6,918.527 km
Eccentricity
0.00013
Inclination
97.7167°
RAAN
59.646°
Arg. of periapsis
314.6653°
True anomaly
45.4574°
Mean anomaly
45.4465°
Eccentric anomaly
45.45195°
Mean motion
3.77157 °/min
Orbital period
95.45 mins
BSTAR
0.001169
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Other satellites on launch #149 in the year 2024 (2024-08-16 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.LEMUR 2 AHMED-ASRAR 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 | 2025-12-07 17:16:59.165Z | 58.493° ENE | 2025-12-07 17:18:59.165Z | 90.739° ESE | 14.865° | 2025-12-07 17:20:59.165Z | 124.28° SE |
| 5 mins | 2025-12-07 18:51:59.165Z | 337.045° NNW | 2025-12-07 18:53:59.165Z | 281.406° WNW | 29.681° | 2025-12-07 18:56:59.165Z | 224.492° SW |
| 6 mins | 2025-12-08 05:33:59.165Z | 174.808° S | 2025-12-08 05:36:59.165Z | 287.436° WNW | 43.435° | 2025-12-08 05:39:59.165Z | 342.584° N |
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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