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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 LEMUR 2 LLOYD
1 60577U 24149DP 26260.48287883 .00007741 00000-0 47044-3 0 9990
2 60577 97.6691 341.7376 0003810 171.1651 188.9646 15.10749767114320Epoch: 2026-09-17T11:35Z
TLE epoch observation values (Epoch: 2026-09-17T11:35:20.730Z)
Latitude
-0.00006°
Longitude
171.48176°
Altitude
539.584 km
Speed
7.591 km/s
True Right ascension
22h 46m 57s
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
16:57:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
533.534 km
Perigee altitude
528.269 km
Semi-major axis
6,909.039 km
Eccentricity
0.00038
Inclination
97.6691°
RAAN
341.7376°
Arg. of periapsis
171.1651°
True anomaly
188.9578°
Mean anomaly
188.9646°
Eccentric anomaly
188.9612°
Mean motion
3.77935 °/min
Orbital period
95.25 mins
BSTAR
0.00047044
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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 | 2026-09-18 05:12:06.285Z | 146.426° SSE | 2026-09-18 05:15:06.285Z | 89.608° E | 47.05° | 2026-09-18 05:19:06.285Z | 359.536° N |
| 6 mins | 2026-09-18 18:22:06.285Z | 15.491° NNE | 2026-09-18 18:24:06.285Z | 32.166° NE | 69.09° | 2026-09-18 18:28:06.285Z | 190.516° SSW |
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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