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, 14.5 m
Radar Cross Section
0.065 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 LEMUR 2 THERMORAPTOR
1 63354U 25061D 25359.43844036 .00004248 00000-0 24758-3 0 9998
2 63354 97.5516 331.8900 0020957 131.2123 229.0918 15.12341798 41339Epoch: 2025-12-25T10:31Z
TLE epoch observation values (Epoch: 2025-12-25T10:31:21.247Z)
Latitude
-0.00004°
Longitude
79.858°
Altitude
541.635 km
Speed
7.586 km/s
True Right ascension
22h 07m 33s
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
00:11:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
540.512 km
Perigee altitude
511.574 km
Semi-major axis
6,904.18 km
Eccentricity
0.0021
Inclination
97.5516°
RAAN
331.89°
Arg. of periapsis
131.2123°
True anomaly
228.91062°
Mean anomaly
229.0918°
Eccentric anomaly
229.00118°
Mean motion
3.78334 °/min
Orbital period
95.15 mins
BSTAR
0.00024758
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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
Loading observer location...
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 | 2025-12-26 10:54:18.307Z | 25.14° NE | 2025-12-26 10:57:18.307Z | 84.629° E | 36.593° | 2025-12-26 11:00:18.307Z | 171.197° S |
| 4 mins | 2025-12-26 21:37:18.307Z | 102.308° ESE | 2025-12-26 21:38:18.307Z | 81.18° E | 20.907° | 2025-12-26 21:41:18.307Z | 21.737° NNE |
| 4 mins | 2025-12-26 23:11:18.307Z | 228.756° WSW | 2025-12-26 23:13:18.307Z | 272.276° WNW | 20.643° | 2025-12-26 23:15:18.307Z | 309.713° 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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