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 8U, 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
0.070 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 LEMUR 2 TILLINFINITY
1 63356U 25061F 26312.17571410 .00005761 00000-0 30449-3 0 9999
2 63356 97.5789 287.5834 0019431 107.7985 252.5369 15.15720480 89442Epoch: 2026-11-08T04:13Z
TLE epoch observation values (Epoch: 2026-11-08T04:13:01.698Z)
Latitude
-0.00004°
Longitude
176.95595°
Altitude
525.918 km
Speed
7.598 km/s
True Right ascension
19h 10m 20s
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
23:50:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
529.167 km
Perigee altitude
502.376 km
Semi-major axis
6,893.908 km
Eccentricity
0.00194
Inclination
97.5789°
RAAN
287.5834°
Arg. of periapsis
107.7985°
True anomaly
252.32465°
Mean anomaly
252.5369°
Eccentric anomaly
252.43076°
Mean motion
3.7918 °/min
Orbital period
94.94 mins
BSTAR
0.00030449
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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 | 2026-11-09 10:53:13.320Z | 33.31° NE | 2026-11-09 10:56:13.320Z | 94.835° ESE | 34.373° | 2026-11-09 10:59:13.320Z | 161.152° S |
| 5 mins | 2026-11-09 23:08:13.320Z | 215.207° SW | 2026-11-09 23:10:13.320Z | 268.637° W | 31.123° | 2026-11-09 23:13:13.320Z | 325.407° NNW |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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