LEMUR 2 STELLA, 60533
Orbit data source: Space-Track
LEMUR 2 STELLA, 60533 is a payload satellite owned by Spire (US) 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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60533 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 STELLA
1 60533U 24149BT 26311.18379605 .00016862 00000-0 91728-3 0 9992
2 60533 97.6672 34.4779 0000979 115.7472 244.3861 15.14533407122121Epoch: 2026-11-07T04:24Z
TLE epoch observation values (Epoch: 2026-11-07T04:24:39.978Z)
Latitude
0.00001°
Longitude
-78.08138°
Altitude
525.763 km
Speed
7.6 km/s
True Right ascension
02h 17m 54s
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
09:58:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
520.055 km
Perigee altitude
518.705 km
Semi-major axis
6,897.517 km
Eccentricity
0.0001
Inclination
97.6672°
RAAN
34.4779°
Arg. of periapsis
115.7472°
True anomaly
244.37598°
Mean anomaly
244.3861°
Eccentric anomaly
244.38104°
Mean motion
3.78882 °/min
Orbital period
95.02 mins
BSTAR
0.00091728
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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 STELLA 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-11-07 17:41:19.837Z | 61.493° ENE | 2026-11-07 17:43:19.837Z | 99.239° ESE | 17.737° | 2026-11-07 17:45:19.837Z | 133.631° SE |
| 5 mins | 2026-11-07 19:15:19.837Z | 334.755° NNW | 2026-11-07 19:17:19.837Z | 287.072° WNW | 28.516° | 2026-11-07 19:20:19.837Z | 230.678° WSW |
| 5 mins | 2026-11-08 05:55:19.837Z | 182.325° SSW | 2026-11-08 05:57:19.837Z | 254.331° W | 65.958° | 2026-11-08 06:00:19.837Z | 339.7° N |
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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