LEMUR 2 THERMORAPTOR, 63354
Orbit data source: Space-Track
LEMUR 2 THERMORAPTOR, 63354 is a payload satellite owned by OroraTech (US) in SSO that was launched on Wed, 26 Mar 2025 UTC via an ELECTRON launch vehicle from the Rocket Lab Launch Complex (RLLC). 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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63354 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~15 kg wet, ~15 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 14.5 m
Radar Cross Section
0.065 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 LEMUR 2 THERMORAPTOR
1 63354U 25061D 26086.90142892 .00004307 00000-0 24376-3 0 9991
2 63354 97.5636 63.4906 0019381 170.9210 189.2376 15.13423320 55313Epoch: 2026-03-27T21:38Z
TLE epoch observation values (Epoch: 2026-03-27T21:38:03.458Z)
Latitude
0.00002°
Longitude
-86.35319°
Altitude
542.057 km
Speed
7.584 km/s
True Right ascension
04h 13m 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
13:13:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
536.125 km
Perigee altitude
509.376 km
Semi-major axis
6,900.888 km
Eccentricity
0.00194
Inclination
97.5636°
RAAN
63.4906°
Arg. of periapsis
170.921°
True anomaly
189.20203°
Mean anomaly
189.2376°
Eccentric anomaly
189.21981°
Mean motion
3.78604 °/min
Orbital period
95.09 mins
BSTAR
0.00024376
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Other satellites on launch #61 in the year 2025 (2025-03-26 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 THERMORAPTOR 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 | 2026-03-28 10:53:17.369Z | 25.193° NE | 2026-03-28 10:57:17.369Z | 121.066° SE | 34.185° | 2026-03-28 11:00:17.369Z | 172.599° S |
| 4 mins | 2026-03-28 21:36:17.369Z | 97.282° ESE | 2026-03-28 21:37:17.369Z | 76.225° E | 20.025° | 2026-03-28 21:40:17.369Z | 21.179° NNE |
| 4 mins | 2026-03-28 23:10:17.369Z | 231.246° WSW | 2026-03-28 23:11:17.369Z | 253.485° W | 22.195° | 2026-03-28 23:14:17.369Z | 314.401° 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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