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: 16 hours ago
TLE from 16 hours ago
0 LEMUR 2 THERMORAPTOR
1 63354U 25061D 25309.67355785 .00006003 00000-0 35471-3 0 9992
2 63354 97.5454 282.7108 0018505 310.7877 49.1748 15.11724178 33812Epoch: 2025-11-05T16:09Z
TLE epoch observation values (Epoch: 2025-11-05T16:09:55.398Z)
Latitude
0.00009°
Longitude
-4.91289°
Altitude
525.67 km
Speed
7.605 km/s
True Right ascension
18h 50m 50s
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
04:02:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
540.704 km
Perigee altitude
515.145 km
Semi-major axis
6,906.061 km
Eccentricity
0.00185
Inclination
97.5454°
RAAN
282.7108°
Arg. of periapsis
310.7877°
True anomaly
49.3355°
Mean anomaly
49.1748°
Eccentric anomaly
49.25513°
Mean motion
3.78179 °/min
Orbital period
95.19 mins
BSTAR
0.00035471
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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 | 2025-11-06 10:13:38.626Z | 57.037° ENE | 2025-11-06 10:15:38.626Z | 89.846° E | 15.657° | 2025-11-06 10:17:38.626Z | 124.611° SE |
| 5 mins | 2025-11-06 11:48:38.626Z | 331.853° NNW | 2025-11-06 11:50:38.626Z | 274.829° WNW | 28.073° | 2025-11-06 11:53:38.626Z | 224.481° SW |
| 5 mins | 2025-11-06 22:29:38.626Z | 177.346° S | 2025-11-06 22:31:38.626Z | 286.564° WNW | 43.776° | 2025-11-06 22:34:38.626Z | 343.41° 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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