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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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 LANGER2SPACE
1 63358U 25061H 26042.48812266 .00006126 00000-0 34800-3 0 9993
2 63358 97.5488 19.1914 0016343 337.8124 22.2398 15.13164576 48601Epoch: 2026-02-11T11:42Z
TLE epoch observation values (Epoch: 2026-02-11T11:42:53.797Z)
Latitude
-0.00004°
Longitude
61.91373°
Altitude
519.189 km
Speed
7.61 km/s
True Right ascension
01h 16m 45s
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
05:53:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
534.817 km
Perigee altitude
512.258 km
Semi-major axis
6,901.674 km
Eccentricity
0.00163
Inclination
97.5488°
RAAN
19.1914°
Arg. of periapsis
337.8124°
True anomaly
22.31082°
Mean anomaly
22.2398°
Eccentric anomaly
22.27529°
Mean motion
3.7854 °/min
Orbital period
95.1 mins
BSTAR
0.000348
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-02-12 10:30:49.832Z | 46.332° ENE | 2026-02-12 10:32:49.832Z | 83.215° E | 22.597° | 2026-02-12 10:35:49.832Z | 145.841° SSE |
| 4 mins | 2026-02-12 12:05:49.832Z | 323.861° NNW | 2026-02-12 12:07:49.832Z | 281.883° WNW | 19.649° | 2026-02-12 12:09:49.832Z | 246.919° WSW |
| 6 mins | 2026-02-12 22:45:49.832Z | 195.447° SSW | 2026-02-12 22:47:49.832Z | 241.334° WSW | 34.021° | 2026-02-12 22:51:49.832Z | 334.452° 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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