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 8U, 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: 3 days ago
TLE from 3 days ago
0 LEMUR 2 KREMPEL-BRO2
1 63353U 25061C 26154.74187176 .00004793 00000-0 26747-3 0 9995
2 63353 97.5687 130.8100 0017791 306.7841 53.1757 15.13900723 65573Epoch: 2026-06-03T17:48Z
TLE epoch observation values (Epoch: 2026-06-03T17:48:17.720Z)
Latitude
0°
Longitude
-28.45996°
Altitude
520.047 km
Speed
7.607 km/s
True Right ascension
08h 43m 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
02:05:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
533.574 km
Perigee altitude
509.024 km
Semi-major axis
6,899.436 km
Eccentricity
0.00178
Inclination
97.5687°
RAAN
130.81°
Arg. of periapsis
306.7841°
True anomaly
53.33911°
Mean anomaly
53.1757°
Eccentric anomaly
53.25738°
Mean motion
3.78724 °/min
Orbital period
95.06 mins
BSTAR
0.00026747
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-06 22:04:10.706Z | 146.774° SSE | 2026-06-06 22:08:10.706Z | 51.109° ENE | 34.531° | 2026-06-06 22:11:10.706Z | 1.367° NNE |
| 5 mins | 2026-06-07 11:13:10.706Z | 18.672° NNE | 2026-06-07 11:15:10.706Z | 85.004° E | 44.232° | 2026-06-07 11:18:10.706Z | 187.27° SSW |
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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