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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Edit Public Description
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, 0.2 m
Radar Cross Section
0.065 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 LEMUR 2 THERMORAPTOR
1 63354U 25061D 25260.87695891 .00005673 00000-0 34303-3 0 9990
2 63354 97.5378 234.5780 0022293 111.4951 248.8659 15.10843227 26442Epoch: 2025-09-17T21:02Z
TLE epoch observation values (Epoch: 2025-09-17T21:02:49.249Z)
Latitude
-0°
Longitude
-78.17381°
Altitude
542.288 km
Speed
7.588 km/s
True Right ascension
15h 38m 18s
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
01:47:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
546.012 km
Perigee altitude
515.209 km
Semi-major axis
6,908.748 km
Eccentricity
0.00223
Inclination
97.5378°
RAAN
234.578°
Arg. of periapsis
111.4951°
True anomaly
248.62786°
Mean anomaly
248.8659°
Eccentric anomaly
248.74686°
Mean motion
3.77959 °/min
Orbital period
95.25 mins
BSTAR
0.00034303
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-09-18 10:21:04.452Z | 56.986° ENE | 2025-09-18 10:23:04.452Z | 94.693° ESE | 17.961° | 2025-09-18 10:25:04.452Z | 132.152° SE |
| 4 mins | 2025-09-18 11:56:04.452Z | 323.691° NNW | 2025-09-18 11:57:04.452Z | 299.972° NW | 23.455° | 2025-09-18 12:00:04.452Z | 236.948° WSW |
| 5 mins | 2025-09-18 22:37:04.452Z | 186.777° SSW | 2025-09-18 22:39:04.452Z | 244.292° WSW | 40.13° | 2025-09-18 22:42:04.452Z | 336.222° NNW |
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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