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 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: 17 hours ago
TLE from 17 hours ago
0 LEMUR 2 LANGER2SPACE
1 63358U 25061H 26264.86890535 .00002721 00000-0 14948-3 0 9994
2 63358 97.5731 240.0649 0014771 285.9532 74.0073 15.14892716 82250Epoch: 2026-09-21T20:51Z
TLE epoch observation values (Epoch: 2026-09-21T20:51:13.422Z)
Latitude
0.00007°
Longitude
-73.48359°
Altitude
521.588 km
Speed
7.604 km/s
True Right ascension
16h 00m 15s
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
06:48:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
528.471 km
Perigee altitude
508.097 km
Semi-major axis
6,896.421 km
Eccentricity
0.00148
Inclination
97.5731°
RAAN
240.0649°
Arg. of periapsis
285.9532°
True anomaly
74.17009°
Mean anomaly
74.0073°
Eccentric anomaly
74.08869°
Mean motion
3.78972 °/min
Orbital period
94.99 mins
BSTAR
0.00014948
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-09-22 22:20:38.179Z | 157.88° S | 2026-09-22 22:23:38.179Z | 95.912° ESE | 68.445° | 2026-09-22 22:26:38.179Z | 354.819° N |
| 6 mins | 2026-09-23 11:28:38.179Z | 4.057° NNE | 2026-09-23 11:30:38.179Z | 317.204° NNW | 68.574° | 2026-09-23 11:34:38.179Z | 200.127° SSW |
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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