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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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, 0.4 m
Radar Cross Section
0.065 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 LEMUR 2 UNTITLED-SC
1 63351U 25061A 25346.87702163 .00007087 00000-0 41804-3 0 9998
2 63351 97.5437 319.0754 0019207 182.1859 177.9291 15.11709316 39425Epoch: 2025-12-12T21:02Z
TLE epoch observation values (Epoch: 2025-12-12T21:02:54.668Z)
Latitude
0°
Longitude
-78.46473°
Altitude
547.327 km
Speed
7.581 km/s
True Right ascension
21h 16m 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
22:22:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
541.234 km
Perigee altitude
514.705 km
Semi-major axis
6,906.107 km
Eccentricity
0.00192
Inclination
97.5437°
RAAN
319.0754°
Arg. of periapsis
182.1859°
True anomaly
177.93703°
Mean anomaly
177.9291°
Eccentric anomaly
177.93307°
Mean motion
3.78175 °/min
Orbital period
95.19 mins
BSTAR
0.00041804
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-12-14 10:10:36.139Z | 59.857° ENE | 2025-12-14 10:12:36.139Z | 93.074° ESE | 14.21° | 2025-12-14 10:14:36.139Z | 126.19° SE |
| 4 mins | 2025-12-14 11:45:36.139Z | 330.462° NNW | 2025-12-14 11:46:36.139Z | 303.716° NW | 28.299° | 2025-12-14 11:49:36.139Z | 229.48° WSW |
| 6 mins | 2025-12-14 22:25:36.139Z | 171.864° S | 2025-12-14 22:28:36.139Z | 309.149° NW | 43.897° | 2025-12-14 22:31:36.139Z | 344.927° 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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