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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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, 14.5 m
Radar Cross Section
0.065 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 22 hours ago
TLE from 22 hours ago
0 LEMUR 2 KREMPEL-BRO2
1 63353U 25061C 25304.65100301 .00008364 00000-0 49382-3 0 9994
2 63353 97.5443 277.7160 0019213 330.5480 29.4666 15.11618964 33059Epoch: 2025-10-31T15:37Z
TLE epoch observation values (Epoch: 2025-10-31T15:37:26.660Z)
Latitude
-0.00001°
Longitude
3.16254°
Altitude
522.783 km
Speed
7.608 km/s
True Right ascension
18h 30m 51s
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
09:06:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
541.514 km
Perigee altitude
514.976 km
Semi-major axis
6,906.382 km
Eccentricity
0.00192
Inclination
97.5443°
RAAN
277.716°
Arg. of periapsis
330.548°
True anomaly
29.57513°
Mean anomaly
29.4666°
Eccentric anomaly
29.52084°
Mean motion
3.78153 °/min
Orbital period
95.2 mins
BSTAR
0.00049382
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-01 21:56:39.156Z | 139.259° SSE | 2025-11-01 21:59:39.156Z | 66.649° ENE | 33.152° | 2025-11-01 22:02:39.156Z | 5.252° NNE |
| 6 mins | 2025-11-02 11:05:39.156Z | 19.711° NNE | 2025-11-02 11:08:39.156Z | 152.301° SSE | 41.558° | 2025-11-02 11:11:39.156Z | 185.707° SSW |
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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