LEMUR 2 LLOYD, 60577
Orbit data source: Space-Track
LEMUR 2 LLOYD, 60577 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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60577 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: 18 hours ago
TLE from 18 hours ago
0 LEMUR 2 LLOYD
1 60577U 24149DP 25338.64068451 .00026680 00000-0 18984-2 0 9994
2 60577 97.6931 55.1566 0004882 92.2493 267.9292 15.04601118 71092Epoch: 2025-12-04T15:22Z
TLE epoch observation values (Epoch: 2025-12-04T15:22:35.141Z)
Latitude
-0.00003°
Longitude
110.81596°
Altitude
555.915 km
Speed
7.584 km/s
True Right ascension
03h 40m 37s
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
07:17:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
553.111 km
Perigee altitude
546.347 km
Semi-major axis
6,927.866 km
Eccentricity
0.00049
Inclination
97.6931°
RAAN
55.1566°
Arg. of periapsis
92.2493°
True anomaly
267.87329°
Mean anomaly
267.9292°
Eccentric anomaly
267.90125°
Mean motion
3.76395 °/min
Orbital period
95.64 mins
BSTAR
0.0018984
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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 LLOYD 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 | 2025-12-05 17:29:26.405Z | 41.381° NE | 2025-12-05 17:32:26.405Z | 101.926° ESE | 25.112° | 2025-12-05 17:35:26.405Z | 155.212° SSE |
| 4 mins | 2025-12-05 19:05:26.405Z | 319.658° NNW | 2025-12-05 19:06:26.405Z | 300.399° NW | 18.608° | 2025-12-05 19:09:26.405Z | 247.307° WSW |
| 5 mins | 2025-12-06 05:49:26.405Z | 210.918° SW | 2025-12-06 05:51:26.405Z | 266.272° W | 30.405° | 2025-12-06 05:54:26.405Z | 326.397° NNW |
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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