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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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, 0.3 m
Radar Cross Section
0.065 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 LEMUR 2 KREMPEL-BRO1
1 63357U 25061G 25309.46435112 .00005509 00000-0 32161-3 0 9998
2 63357 97.5367 282.4171 0017947 304.6824 55.2714 15.12206982 33795Epoch: 2025-11-05T11:08Z
TLE epoch observation values (Epoch: 2025-11-05T11:08:39.936Z)
Latitude
-0.00013°
Longitude
70.31407°
Altitude
525.498 km
Speed
7.604 km/s
True Right ascension
18h 49m 40s
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
04:03:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
538.844 km
Perigee altitude
514.061 km
Semi-major axis
6,904.59 km
Eccentricity
0.00179
Inclination
97.5367°
RAAN
282.4171°
Arg. of periapsis
304.6824°
True anomaly
55.44064°
Mean anomaly
55.2714°
Eccentric anomaly
55.356°
Mean motion
3.783 °/min
Orbital period
95.16 mins
BSTAR
0.00032161
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-11-06 11:32:37.847Z | 351.197° N | 2025-11-06 11:34:37.847Z | 289.93° WNW | 37.77° | 2025-11-06 11:37:37.847Z | 213.624° SW |
| 5 mins | 2025-11-06 22:13:37.847Z | 152.848° SSE | 2025-11-06 22:15:37.847Z | 81.465° E | 42.831° | 2025-11-06 22:18:37.847Z | 355.135° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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