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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Edit Public Description
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: 8 hours ago
TLE from 8 hours ago
0 LEMUR 2 KREMPEL-BRO1
1 63357U 25061G 25297.75166035 .00007629 00000-0 44536-3 0 9995
2 63357 97.5354 270.8582 0019190 346.6756 13.3965 15.12057808 32029Epoch: 2025-10-24T18:02Z
TLE epoch observation values (Epoch: 2025-10-24T18:02:23.454Z)
Latitude
-0.00002°
Longitude
-33.13158°
Altitude
520.104 km
Speed
7.61 km/s
True Right ascension
18h 03m 25s
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
21:13:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
540.158 km
Perigee altitude
513.656 km
Semi-major axis
6,905.044 km
Eccentricity
0.00192
Inclination
97.5354°
RAAN
270.8582°
Arg. of periapsis
346.6756°
True anomaly
13.44757°
Mean anomaly
13.3965°
Eccentric anomaly
13.42202°
Mean motion
3.78263 °/min
Orbital period
95.17 mins
BSTAR
0.00044536
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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 | 2025-10-25 10:30:13.514Z | 47.43° ENE | 2025-10-25 10:32:13.514Z | 85.563° E | 22.952° | 2025-10-25 10:35:13.514Z | 146.879° SSE |
| 4 mins | 2025-10-25 12:05:13.514Z | 323.384° NNW | 2025-10-25 12:07:13.514Z | 281.376° WNW | 19.709° | 2025-10-25 12:09:13.514Z | 246.734° WSW |
| 5 mins | 2025-10-25 22:46:13.514Z | 202.446° SSW | 2025-10-25 22:48:13.514Z | 268.527° W | 34.477° | 2025-10-25 22:51:13.514Z | 331.716° 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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