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: 1 day ago
TLE from 1 day ago
0 LEMUR 2 KREMPEL-BRO2
1 63353U 25061C 25318.41894756 .00007583 00000-0 44578-3 0 9991
2 63353 97.5457 291.3098 0018336 278.9329 80.9826 15.11822628 35133Epoch: 2025-11-14T10:03Z
TLE epoch observation values (Epoch: 2025-11-14T10:03:17.069Z)
Latitude
0.00004°
Longitude
86.72595°
Altitude
531.754 km
Speed
7.598 km/s
True Right ascension
19h 25m 14s
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
10:18:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
540.287 km
Perigee altitude
514.962 km
Semi-major axis
6,905.761 km
Eccentricity
0.00183
Inclination
97.5457°
RAAN
291.3098°
Arg. of periapsis
278.9329°
True anomaly
81.19019°
Mean anomaly
80.9826°
Eccentric anomaly
81.08639°
Mean motion
3.78204 °/min
Orbital period
95.19 mins
BSTAR
0.00044578
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-15 22:43:15.000Z | 191.595° SSW | 2025-11-15 22:46:15.000Z | 282.288° WNW | 35.623° | 2025-11-15 22:49:15.000Z | 334.605° NNW |
| 5 mins | 2025-11-16 11:52:15.000Z | 337.18° NNW | 2025-11-16 11:54:15.000Z | 292.178° WNW | 26.134° | 2025-11-16 11:57:15.000Z | 231.845° WSW |
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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