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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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: 8 hours ago
TLE from 8 hours ago
0 LEMUR 2 LLOYD
1 60577U 24149DP 26126.12838043 .00008855 00000-0 57249-3 0 9997
2 60577 97.6736 207.2638 0002344 293.6018 66.4964 15.08439214 94055Epoch: 2026-05-06T03:04Z
TLE epoch observation values (Epoch: 2026-05-06T03:04:52.069Z)
Latitude
0.00002°
Longitude
-62.94647°
Altitude
543.389 km
Speed
7.591 km/s
True Right ascension
13h 49m 03s
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
19:19:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
539.583 km
Perigee altitude
536.34 km
Semi-major axis
6,916.099 km
Eccentricity
0.00023
Inclination
97.6736°
RAAN
207.2638°
Arg. of periapsis
293.6018°
True anomaly
66.52103°
Mean anomaly
66.4964°
Eccentric anomaly
66.50872°
Mean motion
3.77356 °/min
Orbital period
95.4 mins
BSTAR
0.00057249
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-05-06 17:58:30.085Z | 24.33° NE | 2026-05-06 18:01:30.085Z | 82.365° E | 37.993° | 2026-05-06 18:05:30.085Z | 177.556° S |
| 5 mins | 2026-05-07 04:42:30.085Z | 113.815° SE | 2026-05-07 04:44:30.085Z | 70.588° E | 23.678° | 2026-05-07 04:47:30.085Z | 15.443° NNE |
| 4 mins | 2026-05-07 06:17:30.085Z | 234.357° WSW | 2026-05-07 06:19:30.085Z | 275.918° WNW | 19.01° | 2026-05-07 06:21:30.085Z | 309.83° NW |
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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