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, 0.2 m
Radar Cross Section
0.065 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 LEMUR 2 KREMPEL-BRO2
1 63353U 25061C 25260.88362266 .00005747 00000-0 34787-3 0 9995
2 63353 97.5370 234.5551 0022546 112.5730 247.7889 15.10792344 26443Epoch: 2025-09-17T21:12Z
TLE epoch observation values (Epoch: 2025-09-17T21:12:24.997Z)
Latitude
0.00001°
Longitude
-80.60223°
Altitude
542.779 km
Speed
7.588 km/s
True Right ascension
15h 38m 13s
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
04:05:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
546.343 km
Perigee altitude
515.189 km
Semi-major axis
6,908.903 km
Eccentricity
0.00225
Inclination
97.537°
RAAN
234.5551°
Arg. of periapsis
112.573°
True anomaly
247.54997°
Mean anomaly
247.7889°
Eccentric anomaly
247.66941°
Mean motion
3.77946 °/min
Orbital period
95.25 mins
BSTAR
0.00034787
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-09-18 12:04:49.491Z | 331.169° NNW | 2025-09-18 12:06:49.491Z | 292.958° NW | 19.296° | 2025-09-18 12:08:49.491Z | 253.187° W |
| 5 mins | 2025-09-18 22:46:49.491Z | 201.16° SSW | 2025-09-18 22:48:49.491Z | 260.845° W | 34.339° | 2025-09-18 22:51:49.491Z | 330.278° NNW |
| 4 mins | 2025-09-19 10:21:49.491Z | 65.073° ENE | 2025-09-19 10:22:49.491Z | 84.448° E | 17.783° | 2025-09-19 10:25:49.491Z | 139.135° 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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