LEMUR 2 KREMPEL-BRO1, 63357
Orbit data source: Space-Track
LEMUR 2 KREMPEL-BRO1, 63357 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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63357 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, 0.3 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 KREMPEL-BRO1
1 63357U 25061G 26042.48694235 .00006142 00000-0 34562-3 0 9999
2 63357 97.5484 19.3246 0018164 327.9842 32.0285 15.13480918 48612Epoch: 2026-02-11T11:41Z
TLE epoch observation values (Epoch: 2026-02-11T11:41:11.819Z)
Latitude
0.00008°
Longitude
62.47299°
Altitude
518.044 km
Speed
7.61 km/s
True Right ascension
01h 17m 17s
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
05:54:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
535.109 km
Perigee altitude
510.04 km
Semi-major axis
6,900.712 km
Eccentricity
0.00182
Inclination
97.5484°
RAAN
19.3246°
Arg. of periapsis
327.9842°
True anomaly
32.1391°
Mean anomaly
32.0285°
Eccentric anomaly
32.08378°
Mean motion
3.78619 °/min
Orbital period
95.08 mins
BSTAR
0.00034562
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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 KREMPEL-BRO1 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 10:28:56.732Z | 48.391° ENE | 2026-02-12 10:30:56.732Z | 85.184° E | 21.547° | 2026-02-12 10:33:56.732Z | 144.642° SSE |
| 4 mins | 2026-02-12 12:03:56.732Z | 323.744° NNW | 2026-02-12 12:05:56.732Z | 279.676° WNW | 20.649° | 2026-02-12 12:07:56.732Z | 244.45° WSW |
| 5 mins | 2026-02-12 22:43:56.732Z | 194.558° SSW | 2026-02-12 22:45:56.732Z | 250.835° W | 36.495° | 2026-02-12 22:48:56.732Z | 331.83° 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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