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: 1 day ago
TLE from 1 day ago
0 LEMUR 2 LLOYD
1 60577U 24149DP 25312.83026471 .00019807 00000-0 14438-2 0 9996
2 60577 97.6950 29.4728 0004621 169.6283 190.5039 15.03760195 67213Epoch: 2025-11-08T19:55Z
TLE epoch observation values (Epoch: 2025-11-08T19:55:34.870Z)
Latitude
-0.00001°
Longitude
42.32326°
Altitude
561.525 km
Speed
7.579 km/s
True Right ascension
01h 57m 53s
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
19:07:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
555.517 km
Perigee altitude
549.111 km
Semi-major axis
6,930.451 km
Eccentricity
0.00046
Inclination
97.695°
RAAN
29.4728°
Arg. of periapsis
169.6283°
True anomaly
190.49425°
Mean anomaly
190.5039°
Eccentric anomaly
190.49908°
Mean motion
3.76185 °/min
Orbital period
95.7 mins
BSTAR
0.0014438
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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 | 2025-11-10 05:36:24.395Z | 196.261° SSW | 2025-11-10 05:38:24.395Z | 267.295° W | 37.997° | 2025-11-10 05:41:24.395Z | 334.011° NNW |
| 4 mins | 2025-11-10 17:14:24.395Z | 63.576° ENE | 2025-11-10 17:16:24.395Z | 101.943° ESE | 17.787° | 2025-11-10 17:18:24.395Z | 135.293° SSE |
| 4 mins | 2025-11-10 18:49:24.395Z | 326.255° NNW | 2025-11-10 18:50:24.395Z | 302.625° NW | 25.35° | 2025-11-10 18:53:24.395Z | 236.628° WSW |
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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