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: 17 hours ago
TLE from 17 hours ago
0 LEMUR 2 KREMPEL-BRO2
1 63353U 25061C 25325.89784817 .00004492 00000-0 26507-3 0 9995
2 63353 97.5467 298.6964 0018281 250.4735 109.4521 15.11912128 36260Epoch: 2025-11-21T21:32Z
TLE epoch observation values (Epoch: 2025-11-21T21:32:54.081Z)
Latitude
-0.00006°
Longitude
-85.66321°
Altitude
537.672 km
Speed
7.591 km/s
True Right ascension
19h 54m 47s
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
11:57:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
539.976 km
Perigee altitude
514.728 km
Semi-major axis
6,905.489 km
Eccentricity
0.00183
Inclination
97.5467°
RAAN
298.6964°
Arg. of periapsis
250.4735°
True anomaly
109.64948°
Mean anomaly
109.4521°
Eccentric anomaly
109.5508°
Mean motion
3.78226 °/min
Orbital period
95.18 mins
BSTAR
0.00026507
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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
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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 | 2025-11-22 21:31:45.503Z | 109.337° ESE | 2025-11-22 21:33:45.503Z | 71.89° E | 19.856° | 2025-11-22 21:36:45.503Z | 19.995° NNE |
| 4 mins | 2025-11-22 23:06:45.503Z | 232.205° WSW | 2025-11-22 23:07:45.503Z | 255.54° W | 23.222° | 2025-11-22 23:10:45.503Z | 316.05° NNW |
| 5 mins | 2025-11-23 10:39:45.503Z | 41.23° NE | 2025-11-23 10:41:45.503Z | 81.81° E | 27.368° | 2025-11-23 10:44:45.503Z | 154.143° 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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