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: 11 hours ago
TLE from 11 hours ago
0 LEMUR 2 KREMPEL-BRO2
1 63353U 25061C 25309.88038433 .00006239 00000-0 36890-3 0 9999
2 63353 97.5448 282.8781 0018858 310.9073 49.0524 15.11678205 33846Epoch: 2025-11-05T21:07Z
TLE epoch observation values (Epoch: 2025-11-05T21:07:45.206Z)
Latitude
0.00006°
Longitude
-79.40697°
Altitude
525.63 km
Speed
7.605 km/s
True Right ascension
18h 51m 30s
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
04:04:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
541.088 km
Perigee altitude
515.041 km
Semi-major axis
6,906.202 km
Eccentricity
0.00189
Inclination
97.5448°
RAAN
282.8781°
Arg. of periapsis
310.9073°
True anomaly
49.21587°
Mean anomaly
49.0524°
Eccentric anomaly
49.13411°
Mean motion
3.78168 °/min
Orbital period
95.2 mins
BSTAR
0.0003689
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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 | 2025-11-06 10:25:16.662Z | 49.761° ENE | 2025-11-06 10:27:16.662Z | 85.539° E | 20.5° | 2025-11-06 10:30:16.662Z | 142.649° SSE |
| 4 mins | 2025-11-06 12:00:16.662Z | 326.957° NNW | 2025-11-06 12:02:16.662Z | 282.061° WNW | 22.207° | 2025-11-06 12:04:16.662Z | 244.206° WSW |
| 5 mins | 2025-11-06 22:41:16.662Z | 193.774° SSW | 2025-11-06 22:43:16.662Z | 258.867° W | 38.041° | 2025-11-06 22:46:16.662Z | 334.027° NNW |
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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