LEMUR 2 KREMPEL-BRO2, 63353
Orbit data source: Space-Track
LEMUR 2 KREMPEL-BRO2, 63353 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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63353 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, 14.5 m
Radar Cross Section
0.065 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 LEMUR 2 KREMPEL-BRO2
1 63353U 25061C 26005.49775002 .00005581 00000-0 32302-3 0 9993
2 63353 97.5518 342.7821 0021721 97.2496 263.1205 15.12442917 43006Epoch: 2026-01-05T11:56Z
TLE epoch observation values (Epoch: 2026-01-05T11:56:45.601Z)
Latitude
-0.00001°
Longitude
58.49804°
Altitude
533.658 km
Speed
7.595 km/s
True Right ascension
22h 51m 07s
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
11:39:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
540.731 km
Perigee altitude
510.739 km
Semi-major axis
6,903.872 km
Eccentricity
0.00217
Inclination
97.5518°
RAAN
342.7821°
Arg. of periapsis
97.2496°
True anomaly
262.87347°
Mean anomaly
263.1205°
Eccentric anomaly
262.99698°
Mean motion
3.78359 °/min
Orbital period
95.15 mins
BSTAR
0.00032302
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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-BRO2 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 | 2026-01-07 12:09:04.998Z | 325.718° NNW | 2026-01-07 12:11:04.998Z | 286.64° WNW | 17.875° | 2026-01-07 12:13:04.998Z | 251.126° W |
| 5 mins | 2026-01-07 22:50:04.998Z | 203.759° SW | 2026-01-07 22:52:04.998Z | 260.072° W | 32.411° | 2026-01-07 22:55:04.998Z | 328.447° NNW |
| 4 mins | 2026-01-08 10:24:04.998Z | 60.027° ENE | 2026-01-08 10:26:04.998Z | 100.749° ESE | 18.716° | 2026-01-08 10:28:04.998Z | 136.993° SSE |
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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