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 26099.23744132 .00003739 00000-0 20717-3 0 9991
2 63356 97.5570 75.6588 0019808 122.7238 237.5907 15.14261566 57202Epoch: 2026-04-09T05:41Z
TLE epoch observation values (Epoch: 2026-04-09T05:41:54.930Z)
Latitude
0.00005°
Longitude
152.69158°
Altitude
533.647 km
Speed
7.592 km/s
True Right ascension
05h 02m 38s
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
19:07:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
533.866 km
Perigee altitude
506.537 km
Semi-major axis
6,898.338 km
Eccentricity
0.00198
Inclination
97.557°
RAAN
75.6588°
Arg. of periapsis
122.7238°
True anomaly
237.39933°
Mean anomaly
237.5907°
Eccentric anomaly
237.49499°
Mean motion
3.78814 °/min
Orbital period
95.03 mins
BSTAR
0.00020717
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-04-09 21:42:18.369Z | 119.42° SE | 2026-04-09 21:44:18.369Z | 81.505° E | 22.66° | 2026-04-09 21:47:18.369Z | 19.304° NNE |
| 4 mins | 2026-04-09 23:17:18.369Z | 233.466° WSW | 2026-04-09 23:19:18.369Z | 274.967° WNW | 18.437° | 2026-04-09 23:21:18.369Z | 309.529° NW |
| 4 mins | 2026-04-10 10:50:18.369Z | 50.254° ENE | 2026-04-10 10:51:18.369Z | 78.773° E | 30.725° | 2026-04-10 10:54:18.369Z | 161.219° S |
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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