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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Identifier
Orbit
Country
USRelated business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 8U, 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
0.070 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 LEMUR 2 KREMPEL-BRO2
1 63353U 25061C 26265.16229183 .00002645 00000-0 14647-3 0 9999
2 63353 97.5808 240.6895 0017258 283.8908 76.0404 15.14608025 82287Epoch: 2026-09-22T03:53Z
TLE epoch observation values (Epoch: 2026-09-22T03:53:42.014Z)
Latitude
0.00002°
Longitude
-178.76729°
Altitude
522.393 km
Speed
7.604 km/s
True Right ascension
16h 02m 45s
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
06:48:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
531.053 km
Perigee altitude
507.246 km
Semi-major axis
6,897.286 km
Eccentricity
0.00173
Inclination
97.5808°
RAAN
240.6895°
Arg. of periapsis
283.8908°
True anomaly
76.23242°
Mean anomaly
76.0404°
Eccentric anomaly
76.1364°
Mean motion
3.78901 °/min
Orbital period
95.01 mins
BSTAR
0.00014647
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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 | 2026-09-22 21:29:30.557Z | 103.988° ESE | 2026-09-22 21:31:30.557Z | 71.658° E | 15.977° | 2026-09-22 21:33:30.557Z | 36.587° NE |
| 5 mins | 2026-09-22 23:03:30.557Z | 208.766° SW | 2026-09-22 23:05:30.557Z | 257.917° W | 33.916° | 2026-09-22 23:08:30.557Z | 324.013° NNW |
| 5 mins | 2026-09-23 10:36:30.557Z | 52.785° ENE | 2026-09-23 10:38:30.557Z | 93.153° ESE | 23.322° | 2026-09-23 10:41:30.557Z | 147.834° SSE |
| 4 mins | 2026-09-23 12:11:30.557Z | 316.811° NNW | 2026-09-23 12:12:30.557Z | 294.358° NW | 22.76° | 2026-09-23 12:15:30.557Z | 239.945° 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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