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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60576 intel report (Beta)
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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: 7 hours ago
TLE from 7 hours ago
0 LEMUR 2 AHMED-ASRAR
1 60576U 24149DN 26126.80610508 .00009557 00000-0 56342-3 0 9998
2 60576 97.6988 211.4544 0003415 129.4516 230.7017 15.11787166 94315Epoch: 2026-05-06T19:20Z
TLE epoch observation values (Epoch: 2026-05-06T19:20:47.478Z)
Latitude
0.00001°
Longitude
56.59526°
Altitude
535.316 km
Speed
7.594 km/s
True Right ascension
14h 05m 49s
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
10:26:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
530.098 km
Perigee altitude
525.381 km
Semi-major axis
6,905.876 km
Eccentricity
0.00034
Inclination
97.6988°
RAAN
211.4544°
Arg. of periapsis
129.4516°
True anomaly
230.67142°
Mean anomaly
230.7017°
Eccentric anomaly
230.68656°
Mean motion
3.78194 °/min
Orbital period
95.19 mins
BSTAR
0.00056342
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-05-07 05:00:38.695Z | 130.898° SE | 2026-05-07 05:03:38.695Z | 77.025° E | 25.975° | 2026-05-07 05:06:38.695Z | 14.478° NNE |
| 4 mins | 2026-05-07 06:36:38.695Z | 236.85° WSW | 2026-05-07 06:38:38.695Z | 275.006° WNW | 16.558° | 2026-05-07 06:40:38.695Z | 307.471° NW |
| 6 mins | 2026-05-07 18:09:38.695Z | 30.84° NE | 2026-05-07 18:12:38.695Z | 118.281° SE | 35.117° | 2026-05-07 18:15:38.695Z | 172.712° S |
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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