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: 9 hours ago
TLE from 9 hours ago
0 LEMUR 2 LLOYD
1 60577U 24149DP 26265.18540922 .00006922 00000-0 42043-3 0 9992
2 60577 97.6691 346.4490 0004054 161.0681 199.0700 15.10807216115038Epoch: 2026-09-22T04:26Z
TLE epoch observation values (Epoch: 2026-09-22T04:26:59.356Z)
Latitude
-0.00001°
Longitude
-81.35283°
Altitude
539.456 km
Speed
7.591 km/s
True Right ascension
23h 05m 47s
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
06:10:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
533.527 km
Perigee altitude
527.926 km
Semi-major axis
6,908.863 km
Eccentricity
0.00041
Inclination
97.6691°
RAAN
346.449°
Arg. of periapsis
161.0681°
True anomaly
199.05483°
Mean anomaly
199.07°
Eccentric anomaly
199.06241°
Mean motion
3.77949 °/min
Orbital period
95.25 mins
BSTAR
0.00042043
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-22 17:44:56.759Z | 46.535° ENE | 2026-09-22 17:46:56.759Z | 86.278° E | 26.56° | 2026-09-22 17:49:56.759Z | 149.572° SSE |
| 4 mins | 2026-09-22 19:19:56.759Z | 322.885° NNW | 2026-09-22 19:21:56.759Z | 282.479° WNW | 19.484° | 2026-09-22 19:23:56.759Z | 248.656° W |
| 6 mins | 2026-09-23 06:00:56.759Z | 200.234° SSW | 2026-09-23 06:02:56.759Z | 245.066° WSW | 38.377° | 2026-09-23 06:06:56.759Z | 331.857° 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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