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: 4 hours ago
TLE from 4 hours ago
0 LEMUR 2 LLOYD
1 60577U 24149DP 26035.18859560 .00012178 00000-0 83138-3 0 9998
2 60577 97.6838 116.4875 0003440 231.0292 129.0629 15.06334011 80359Epoch: 2026-02-04T04:31Z
TLE epoch observation values (Epoch: 2026-02-04T04:31:34.659Z)
Latitude
-0.00002°
Longitude
-85.76567°
Altitude
551.98 km
Speed
7.585 km/s
True Right ascension
07h 45m 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
10:40:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
546.791 km
Perigee altitude
542.029 km
Semi-major axis
6,922.547 km
Eccentricity
0.00034
Inclination
97.6838°
RAAN
116.4875°
Arg. of periapsis
231.0292°
True anomaly
129.0935°
Mean anomaly
129.0629°
Eccentric anomaly
129.0782°
Mean motion
3.76829 °/min
Orbital period
95.53 mins
BSTAR
0.00083138
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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 | 2026-02-04 17:50:28.747Z | 24.6° NE | 2026-02-04 17:54:28.747Z | 118.568° SE | 35.952° | 2026-02-04 17:57:28.747Z | 173.171° S |
| 4 mins | 2026-02-05 04:36:28.747Z | 99.861° ESE | 2026-02-05 04:37:28.747Z | 77.106° E | 22.723° | 2026-02-05 04:40:28.747Z | 19.014° NNE |
| 4 mins | 2026-02-05 06:10:28.747Z | 227.091° WSW | 2026-02-05 06:12:28.747Z | 267.489° W | 20.567° | 2026-02-05 06:14:28.747Z | 305.858° NW |
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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