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: 18 hours ago
TLE from 18 hours ago
0 LEMUR 2 LLOYD
1 60577U 24149DP 25286.93857073 .00014219 00000-0 10606-2 0 9992
2 60577 97.6981 3.7390 0002577 250.8031 109.2915 15.02970554 63328Epoch: 2025-10-13T22:31Z
TLE epoch observation values (Epoch: 2025-10-13T22:31:32.511Z)
Latitude
-0.00003°
Longitude
3.11937°
Altitude
561.392 km
Speed
7.58 km/s
True Right ascension
00h 14m 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
10:39:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
556.53 km
Perigee altitude
552.957 km
Semi-major axis
6,932.881 km
Eccentricity
0.00026
Inclination
97.6981°
RAAN
3.739°
Arg. of periapsis
250.8031°
True anomaly
109.31937°
Mean anomaly
109.2915°
Eccentric anomaly
109.30543°
Mean motion
3.75987 °/min
Orbital period
95.75 mins
BSTAR
0.0010606
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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 | 2025-10-14 18:15:49.224Z | 6.264° NNE | 2025-10-14 18:18:49.224Z | 311.661° NW | 42.889° | 2025-10-14 18:22:49.224Z | 201.15° SSW |
| 6 mins | 2025-10-15 05:01:49.224Z | 145.726° SSE | 2025-10-15 05:03:49.224Z | 85.047° E | 40.415° | 2025-10-15 05:07:49.224Z | 355.854° N |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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