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: 7 hours ago
TLE from 7 hours ago
0 LEMUR 2 KREMPEL-BRO2
1 63353U 25061C 26067.87188233 .00009003 00000-0 50902-3 0 9996
2 63353 97.5616 44.5529 0017888 240.7333 119.2110 15.13176125 52430Epoch: 2026-03-08T20:55Z
TLE epoch observation values (Epoch: 2026-03-08T20:55:30.633Z)
Latitude
-0.00003°
Longitude
-75.89769°
Altitude
535.644 km
Speed
7.591 km/s
True Right ascension
02h 58m 12s
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
08:07:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
535.849 km
Perigee altitude
511.157 km
Semi-major axis
6,901.64 km
Eccentricity
0.00179
Inclination
97.5616°
RAAN
44.5529°
Arg. of periapsis
240.7333°
True anomaly
119.38972°
Mean anomaly
119.211°
Eccentric anomaly
119.30038°
Mean motion
3.78543 °/min
Orbital period
95.1 mins
BSTAR
0.00050902
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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 | 2026-03-09 11:47:01.392Z | 341.504° N | 2026-03-09 11:49:01.392Z | 291.368° WNW | 29.794° | 2026-03-09 11:52:01.392Z | 225.623° WSW |
| 6 mins | 2026-03-09 22:27:01.392Z | 170.184° S | 2026-03-09 22:30:01.392Z | 322.855° NNW | 43.936° | 2026-03-09 22:33:01.392Z | 345.945° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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