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: 11 hours ago
TLE from 11 hours ago
0 LEMUR 2 KREMPEL-BRO1
1 63357U 25061G 25359.47807405 .00007002 00000-0 39999-3 0 9998
2 63357 97.5431 331.8218 0020659 124.9402 235.3773 15.12843351 41351Epoch: 2025-12-25T11:28Z
TLE epoch observation values (Epoch: 2025-12-25T11:28:25.597Z)
Latitude
-0.00008°
Longitude
65.48262°
Altitude
538.738 km
Speed
7.589 km/s
True Right ascension
22h 07m 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
22:06:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
538.775 km
Perigee altitude
510.255 km
Semi-major axis
6,902.652 km
Eccentricity
0.00207
Inclination
97.5431°
RAAN
331.8218°
Arg. of periapsis
124.9402°
True anomaly
235.18277°
Mean anomaly
235.3773°
Eccentric anomaly
235.28001°
Mean motion
3.78459 °/min
Orbital period
95.12 mins
BSTAR
0.00039999
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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
Loading observer location...
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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-12-26 11:52:07.081Z | 324.76° NNW | 2025-12-26 11:53:07.081Z | 298.717° NW | 25.575° | 2025-12-26 11:56:07.081Z | 232.752° WSW |
| 5 mins | 2025-12-26 22:32:07.081Z | 179.437° S | 2025-12-26 22:34:07.081Z | 229.622° WSW | 42.416° | 2025-12-26 22:37:07.081Z | 340.183° N |
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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