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 8U, 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: 3 days ago
TLE from 3 days ago
0 LEMUR 2 THERMORAPTOR
1 63354U 25061D 26154.98900498 .00004355 00000-0 24289-3 0 9995
2 63354 97.5694 131.1285 0017367 304.9847 54.9753 15.13981450 65611Epoch: 2026-06-03T23:44Z
TLE epoch observation values (Epoch: 2026-06-03T23:44:10.030Z)
Latitude
-0.00004°
Longitude
-117.353°
Altitude
520.283 km
Speed
7.607 km/s
True Right ascension
08h 44m 30s
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
02:05:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
533.035 km
Perigee altitude
509.072 km
Semi-major axis
6,899.19 km
Eccentricity
0.00174
Inclination
97.5694°
RAAN
131.1285°
Arg. of periapsis
304.9847°
True anomaly
55.13847°
Mean anomaly
54.9753°
Eccentric anomaly
55.05687°
Mean motion
3.78744 °/min
Orbital period
95.05 mins
BSTAR
0.00024289
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-06 21:40:22.931Z | 119.52° SE | 2026-06-06 21:43:22.931Z | 61.927° ENE | 21.314° | 2026-06-06 21:45:22.931Z | 24.245° NE |
| 4 mins | 2026-06-06 23:15:22.931Z | 226.934° WSW | 2026-06-06 23:17:22.931Z | 269.327° W | 20.632° | 2026-06-06 23:19:22.931Z | 307.989° NW |
| 5 mins | 2026-06-07 10:48:22.931Z | 44.735° NE | 2026-06-07 10:50:22.931Z | 97.861° ESE | 30.233° | 2026-06-07 10:53:22.931Z | 161.749° S |
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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