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 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: 16 hours ago
TLE from 16 hours ago
0 LEMUR 2 KREMPEL-BRO2
1 63353U 25061C 26042.47607251 .00006233 00000-0 35640-3 0 9995
2 63353 97.5565 19.3839 0018992 336.0531 23.9815 15.12884257 48599Epoch: 2026-02-11T11:25Z
TLE epoch observation values (Epoch: 2026-02-11T11:25:32.664Z)
Latitude
-0.00001°
Longitude
66.45616°
Altitude
518.504 km
Speed
7.611 km/s
True Right ascension
01h 17m 32s
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
05:52:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
537.5 km
Perigee altitude
511.282 km
Semi-major axis
6,902.528 km
Eccentricity
0.0019
Inclination
97.5565°
RAAN
19.3839°
Arg. of periapsis
336.0531°
True anomaly
24.07015°
Mean anomaly
23.9815°
Eccentric anomaly
24.0258°
Mean motion
3.7847 °/min
Orbital period
95.12 mins
BSTAR
0.0003564
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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 | 2026-02-12 10:14:30.203Z | 62.436° ENE | 2026-02-12 10:16:30.203Z | 97.043° ESE | 15.288° | 2026-02-12 10:18:30.203Z | 129.415° SE |
| 5 mins | 2026-02-12 11:48:30.203Z | 340.731° N | 2026-02-12 11:50:30.203Z | 293.381° NW | 28.86° | 2026-02-12 11:53:30.203Z | 228.05° WSW |
| 5 mins | 2026-02-12 22:29:30.203Z | 175.076° S | 2026-02-12 22:31:30.203Z | 275.659° WNW | 44.274° | 2026-02-12 22:34:30.203Z | 344.095° N |
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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