LEMUR 2 LANGER2SPACE, 63358
Orbit data source: Space-Track
LEMUR 2 LANGER2SPACE, 63358 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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63358 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, 0.2 m
Radar Cross Section
0.065 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 LEMUR 2 LANGER2SPACE
1 63358U 25061H 25260.92144110 .00004851 00000-0 29255-3 0 9990
2 63358 97.5299 234.4750 0020059 113.1199 247.2148 15.11047014 26453Epoch: 2025-09-17T22:06Z
TLE epoch observation values (Epoch: 2025-09-17T22:06:52.511Z)
Latitude
0.00005°
Longitude
-94.33426°
Altitude
541.474 km
Speed
7.589 km/s
True Right ascension
15h 37m 53s
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
03:59:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
543.846 km
Perigee altitude
516.132 km
Semi-major axis
6,908.126 km
Eccentricity
0.00201
Inclination
97.5299°
RAAN
234.475°
Arg. of periapsis
113.1199°
True anomaly
247.00308°
Mean anomaly
247.2148°
Eccentric anomaly
247.10892°
Mean motion
3.7801 °/min
Orbital period
95.24 mins
BSTAR
0.00029255
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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 LANGER2SPACE 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-09-18 11:22:57.972Z | 5.126° NNE | 2025-09-18 11:26:57.972Z | 243.341° WSW | 39.925° | 2025-09-18 11:29:57.972Z | 203.748° SW |
| 5 mins | 2025-09-18 22:05:57.972Z | 143.601° SSE | 2025-09-18 22:07:57.972Z | 84.131° E | 38.859° | 2025-09-18 22:10:57.972Z | 0.878° NNE |
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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