LEMUR 2 TILLINFINITY, 63356
Orbit data source: Space-Track
LEMUR 2 TILLINFINITY, 63356 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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63356 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, 0.2 m
Radar Cross Section
0.065 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 TILLINFINITY
1 63356U 25061F 25260.80698401 .00005633 00000-0 33497-3 0 9994
2 63356 97.5288 234.4576 0021505 105.1465 255.2146 15.11462276 26446Epoch: 2025-09-17T19:22Z
TLE epoch observation values (Epoch: 2025-09-17T19:22:03.418Z)
Latitude
-0°
Longitude
-53.03428°
Altitude
538.638 km
Speed
7.591 km/s
True Right ascension
15h 37m 49s
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
04:01:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
543.575 km
Perigee altitude
513.869 km
Semi-major axis
6,906.859 km
Eccentricity
0.00215
Inclination
97.5288°
RAAN
234.4576°
Arg. of periapsis
105.1465°
True anomaly
254.97649°
Mean anomaly
255.2146°
Eccentric anomaly
255.09553°
Mean motion
3.78114 °/min
Orbital period
95.21 mins
BSTAR
0.00033497
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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 TILLINFINITY 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 | 2025-09-18 11:48:53.990Z | 346.662° N | 2025-09-18 11:51:53.990Z | 283.237° WNW | 26.679° | 2025-09-18 11:54:53.990Z | 227.55° WSW |
| 6 mins | 2025-09-18 22:30:53.990Z | 178.008° S | 2025-09-18 22:32:53.990Z | 217.547° SW | 42.082° | 2025-09-18 22:36:53.990Z | 343.028° N |
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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