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 26098.88446681 .00003846 00000-0 21612-3 0 9995
2 63358 97.5577 75.0853 0018203 133.0621 227.2138 15.13770961 57136Epoch: 2026-04-08T21:13Z
TLE epoch observation values (Epoch: 2026-04-08T21:13:37.932Z)
Latitude
-0.00001°
Longitude
-80.46317°
Altitude
536.339 km
Speed
7.59 km/s
True Right ascension
05h 00m 20s
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
19:06:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
534.253 km
Perigee altitude
509.133 km
Semi-major axis
6,899.83 km
Eccentricity
0.00182
Inclination
97.5577°
RAAN
75.0853°
Arg. of periapsis
133.0621°
True anomaly
227.06095°
Mean anomaly
227.2138°
Eccentric anomaly
227.13735°
Mean motion
3.78692 °/min
Orbital period
95.06 mins
BSTAR
0.00021612
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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 | 2026-04-09 22:44:55.058Z | 195.111° SSW | 2026-04-09 22:46:55.058Z | 251.946° W | 36.39° | 2026-04-09 22:49:55.058Z | 331.712° NNW |
| 4 mins | 2026-04-10 11:52:55.058Z | 329.244° NNW | 2026-04-10 11:54:55.058Z | 274.033° WNW | 25.436° | 2026-04-10 11:56:55.058Z | 234.577° WSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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