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 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: 1 day ago
TLE from 1 day ago
0 LEMUR 2 KREMPEL-BRO1
1 63357U 25061G 26311.90423140 .00005486 00000-0 29174-3 0 9993
2 63357 97.5790 287.1870 0020020 109.8876 250.4516 15.15513891 89390Epoch: 2026-11-07T21:42Z
TLE epoch observation values (Epoch: 2026-11-07T21:42:05.592Z)
Latitude
-0.00003°
Longitude
-85.43909°
Altitude
527.144 km
Speed
7.597 km/s
True Right ascension
19h 08m 44s
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
23:50:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
530.201 km
Perigee altitude
502.595 km
Semi-major axis
6,894.535 km
Eccentricity
0.002
Inclination
97.579°
RAAN
287.187°
Arg. of periapsis
109.8876°
True anomaly
250.23559°
Mean anomaly
250.4516°
Eccentric anomaly
250.34358°
Mean motion
3.79128 °/min
Orbital period
94.95 mins
BSTAR
0.00029174
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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 | 2026-11-09 10:43:13.507Z | 41.658° NE | 2026-11-09 10:46:13.507Z | 103.162° ESE | 25.886° | 2026-11-09 10:48:13.507Z | 144.997° SSE |
| 5 mins | 2026-11-09 22:58:13.507Z | 207.72° SW | 2026-11-09 23:00:13.507Z | 278.932° WNW | 40.17° | 2026-11-09 23:03:13.507Z | 332.32° NNW |
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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