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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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: 6 hours ago
TLE from 6 hours ago
0 LEMUR 2 AHMED-ASRAR
1 60576U 24149DN 25312.15172205 .00017434 00000-0 11777-2 0 9994
2 60576 97.7190 30.8888 0003286 60.7240 299.4315 15.06640097 67219Epoch: 2025-11-08T03:38Z
TLE epoch observation values (Epoch: 2025-11-08T03:38:28.785Z)
Latitude
-0.00001°
Longitude
-71.31658°
Altitude
548.421 km
Speed
7.588 km/s
True Right ascension
02h 03m 33s
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
05:37:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
545.747 km
Perigee altitude
541.199 km
Semi-major axis
6,921.61 km
Eccentricity
0.00033
Inclination
97.719°
RAAN
30.8888°
Arg. of periapsis
60.724°
True anomaly
299.3987°
Mean anomaly
299.4315°
Eccentric anomaly
299.4151°
Mean motion
3.76906 °/min
Orbital period
95.51 mins
BSTAR
0.0011777
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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 | 2025-11-08 18:32:59.284Z | 0.429° NNE | 2025-11-08 18:35:59.284Z | 289.686° WNW | 39.411° | 2025-11-08 18:38:59.284Z | 211.116° SW |
| 6 mins | 2025-11-09 05:16:59.284Z | 155.873° SSE | 2025-11-09 05:18:59.284Z | 122.753° SE | 41.613° | 2025-11-09 05:22:59.284Z | 352.877° N |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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