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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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, 0.4 m
Radar Cross Section
0.065 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 LEMUR 2 TILLINFINITY
1 63356U 25061F 26042.92530712 .00005478 00000-0 30733-3 0 9993
2 63356 97.5487 19.8098 0017307 325.7415 34.2699 15.13647790 48687Epoch: 2026-02-11T22:12Z
TLE epoch observation values (Epoch: 2026-02-11T22:12:26.535Z)
Latitude
0.00004°
Longitude
-95.28519°
Altitude
518.296 km
Speed
7.61 km/s
True Right ascension
01h 19m 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
07:46:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
534.009 km
Perigee altitude
510.125 km
Semi-major axis
6,900.204 km
Eccentricity
0.00173
Inclination
97.5487°
RAAN
19.8098°
Arg. of periapsis
325.7415°
True anomaly
34.38177°
Mean anomaly
34.2699°
Eccentric anomaly
34.32582°
Mean motion
3.78661 °/min
Orbital period
95.07 mins
BSTAR
0.00030733
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-02-12 11:27:05.628Z | 4.048° NNE | 2026-02-12 11:31:05.628Z | 258.321° W | 39.952° | 2026-02-12 11:34:05.628Z | 206.543° SW |
| 5 mins | 2026-02-12 22:09:05.628Z | 144.703° SSE | 2026-02-12 22:11:05.628Z | 79.506° E | 39.673° | 2026-02-12 22:14:05.628Z | 359.519° 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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