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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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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 22 hours ago
TLE from 22 hours ago
0 LEMUR 2 STELLA
1 60533U 24149BT 26034.17775669 .00014074 00000-0 90614-3 0 9999
2 60533 97.6829 116.3364 0001359 121.8120 238.3241 15.08469362 80271Epoch: 2026-02-03T04:15Z
TLE epoch observation values (Epoch: 2026-02-03T04:15:58.178Z)
Latitude
0.00005°
Longitude
-81.01844°
Altitude
544.437 km
Speed
7.59 km/s
True Right ascension
07h 45m 20s
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
04:25:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
538.81 km
Perigee altitude
536.93 km
Semi-major axis
6,916.007 km
Eccentricity
0.00014
Inclination
97.6829°
RAAN
116.3364°
Arg. of periapsis
121.812°
True anomaly
238.31085°
Mean anomaly
238.3241°
Eccentric anomaly
238.31747°
Mean motion
3.77364 °/min
Orbital period
95.4 mins
BSTAR
0.00090614
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-02-04 05:52:09.799Z | 199.982° SSW | 2026-02-04 05:55:09.799Z | 279.875° WNW | 30.933° | 2026-02-04 05:58:09.799Z | 330.369° NNW |
| 4 mins | 2026-02-04 17:29:09.799Z | 69.364° E | 2026-02-04 17:30:09.799Z | 91.47° ESE | 20.778° | 2026-02-04 17:33:09.799Z | 145.781° SSE |
| 4 mins | 2026-02-04 19:03:09.799Z | 325.934° NNW | 2026-02-04 19:05:09.799Z | 280.772° WNW | 21.766° | 2026-02-04 19:07:09.799Z | 243.884° 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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