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, 14.5 m
Radar Cross Section
0.065 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 3 days ago
TLE from 3 days ago
0 LEMUR 2 LANGER2SPACE
1 63358U 25061H 26154.46902708 .00004548 00000-0 25228-3 0 9996
2 63358 97.5611 130.2690 0015293 309.4835 50.5043 15.14181758 65547Epoch: 2026-06-03T11:15Z
TLE epoch observation values (Epoch: 2026-06-03T11:15:23.939Z)
Latitude
-0.00006°
Longitude
69.49206°
Altitude
519.837 km
Speed
7.607 km/s
True Right ascension
08h 41m 04s
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
00:57:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
530.994 km
Perigee altitude
509.894 km
Semi-major axis
6,898.581 km
Eccentricity
0.00153
Inclination
97.5611°
RAAN
130.269°
Arg. of periapsis
309.4835°
True anomaly
50.6397°
Mean anomaly
50.5043°
Eccentric anomaly
50.57198°
Mean motion
3.78794 °/min
Orbital period
95.04 mins
BSTAR
0.00025228
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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 | 2026-06-06 21:51:48.522Z | 132.971° SE | 2026-06-06 21:54:48.522Z | 71.576° E | 28.305° | 2026-06-06 21:57:48.522Z | 10.697° NNE |
| 6 mins | 2026-06-07 10:59:48.522Z | 30.017° NE | 2026-06-07 11:01:48.522Z | 80.682° E | 37.929° | 2026-06-07 11:05:48.522Z | 177.643° S |
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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