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: 15 hours ago
TLE from 15 hours ago
0 LEMUR 2 LLOYD
1 60577U 24149DP 26171.22464490 .00008514 00000-0 53795-3 0 9993
2 60577 97.6744 252.3554 0005125 131.3141 228.8530 15.09289702100852Epoch: 2026-06-20T05:23Z
TLE epoch observation values (Epoch: 2026-06-20T05:23:29.319Z)
Latitude
0.00005°
Longitude
-96.9591°
Altitude
543.771 km
Speed
7.589 km/s
True Right ascension
16h 49m 25s
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
07:19:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
538.904 km
Perigee altitude
531.818 km
Semi-major axis
6,913.498 km
Eccentricity
0.00051
Inclination
97.6744°
RAAN
252.3554°
Arg. of periapsis
131.3141°
True anomaly
228.80879°
Mean anomaly
228.853°
Eccentric anomaly
228.8309°
Mean motion
3.77569 °/min
Orbital period
95.35 mins
BSTAR
0.00053795
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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 | 2026-06-21 05:22:42.326Z | 162.723° S | 2026-06-21 05:26:42.326Z | 10.092° NNE | 42.477° | 2026-06-21 05:29:42.326Z | 350.398° N |
| 6 mins | 2026-06-21 18:33:42.326Z | 358.543° N | 2026-06-21 18:35:42.326Z | 313.055° NW | 39.515° | 2026-06-21 18:39:42.326Z | 206.2° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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