LEMUR 2 KREMPEL-BRO1, 63357
Orbit data source: Space-Track
LEMUR 2 KREMPEL-BRO1, 63357 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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63357 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: 16 hours ago
TLE from 16 hours ago
0 LEMUR 2 KREMPEL-BRO1
1 63357U 25061G 26264.88876602 .00002862 00000-0 15557-3 0 9997
2 63357 97.5725 240.3104 0016617 275.5340 84.3997 15.15207911 82273Epoch: 2026-09-21T21:19Z
TLE epoch observation values (Epoch: 2026-09-21T21:19:49.384Z)
Latitude
0.00003°
Longitude
-80.4075°
Altitude
522.326 km
Speed
7.603 km/s
True Right ascension
16h 01m 14s
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
06:49:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
528.785 km
Perigee altitude
505.869 km
Semi-major axis
6,895.464 km
Eccentricity
0.00166
Inclination
97.5725°
RAAN
240.3104°
Arg. of periapsis
275.534°
True anomaly
84.58925°
Mean anomaly
84.3997°
Eccentric anomaly
84.49447°
Mean motion
3.79051 °/min
Orbital period
94.97 mins
BSTAR
0.00015557
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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-BRO1 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-09-22 22:49:17.478Z | 189.885° SSW | 2026-09-22 22:52:17.478Z | 288.608° WNW | 47.051° | 2026-09-22 22:55:17.478Z | 336.265° NNW |
| 5 mins | 2026-09-23 11:56:17.478Z | 342.459° N | 2026-09-23 11:58:17.478Z | 299.949° NW | 31.577° | 2026-09-23 12:01:17.478Z | 230.839° WSW |
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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