LEMUR 2 UNTITLED-SC, 63351
Orbit data source: Space-Track
LEMUR 2 UNTITLED-SC, 63351 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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63351 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, 0.2 m
Radar Cross Section
0.070 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 22 hours ago
TLE from 22 hours ago
0 LEMUR 2 UNTITLED-SC
1 63351U 25061A 26312.24396632 .00005388 00000-0 29617-3 0 9993
2 63351 97.5820 286.7919 0019832 124.7690 235.5412 15.14348085 89384Epoch: 2026-11-08T05:51Z
TLE epoch observation values (Epoch: 2026-11-08T05:51:18.690Z)
Latitude
0.00001°
Longitude
151.52637°
Altitude
533.8 km
Speed
7.592 km/s
True Right ascension
19h 07m 10s
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
23:50:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
533.62 km
Perigee altitude
506.259 km
Semi-major axis
6,898.076 km
Eccentricity
0.00198
Inclination
97.582°
RAAN
286.7919°
Arg. of periapsis
124.769°
True anomaly
235.35408°
Mean anomaly
235.5412°
Eccentric anomaly
235.44761°
Mean motion
3.78836 °/min
Orbital period
95.03 mins
BSTAR
0.00029617
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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 UNTITLED-SC 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-11-09 10:58:13.851Z | 29.857° NE | 2026-11-09 11:01:13.851Z | 107.698° ESE | 43.89° | 2026-11-09 11:04:13.851Z | 170.624° S |
| 4 mins | 2026-11-09 21:40:13.851Z | 94.804° ESE | 2026-11-09 21:41:13.851Z | 73.563° E | 20.594° | 2026-11-09 21:44:13.851Z | 20.4° NNE |
| 4 mins | 2026-11-09 23:14:13.851Z | 233.745° WSW | 2026-11-09 23:15:13.851Z | 257.558° W | 24.651° | 2026-11-09 23:18:13.851Z | 316.869° 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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