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: 5 hours ago
TLE from 5 hours ago
0 LEMUR 2 KREMPEL-BRO1
1 63357U 25061G 25359.80878622 .00007351 00000-0 41960-3 0 9992
2 63357 97.5432 332.1487 0020706 123.9066 236.4138 15.12849304 41409Epoch: 2025-12-25T19:24Z
TLE epoch observation values (Epoch: 2025-12-25T19:24:39.129Z)
Latitude
-0°
Longitude
-53.57284°
Altitude
538.525 km
Speed
7.589 km/s
True Right ascension
22h 08m 35s
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
00:11:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
538.789 km
Perigee altitude
510.204 km
Semi-major axis
6,902.634 km
Eccentricity
0.00207
Inclination
97.5432°
RAAN
332.1487°
Arg. of periapsis
123.9066°
True anomaly
236.21642°
Mean anomaly
236.4138°
Eccentric anomaly
236.31508°
Mean motion
3.78461 °/min
Orbital period
95.12 mins
BSTAR
0.0004196
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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 10:16:54.578Z | 55.427° ENE | 2025-12-26 10:18:54.578Z | 89.559° E | 15.946° | 2025-12-26 10:20:54.578Z | 126.308° SE |
| 4 mins | 2025-12-26 11:51:54.578Z | 328.799° NNW | 2025-12-26 11:53:54.578Z | 274.059° WNW | 25.209° | 2025-12-26 11:55:54.578Z | 234.916° WSW |
| 6 mins | 2025-12-26 22:31:54.578Z | 178.484° S | 2025-12-26 22:33:54.578Z | 213.022° SW | 41.128° | 2025-12-26 22:37:54.578Z | 342.378° N |
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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