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, 0.4 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 TILLINFINITY
1 63356U 25061F 26154.73780320 .00004738 00000-0 25890-3 0 9994
2 63356 97.5604 130.7967 0016358 296.8475 63.1084 15.14680244 65607Epoch: 2026-06-03T17:42Z
TLE epoch observation values (Epoch: 2026-06-03T17:42:26.196Z)
Latitude
-0.00002°
Longitude
-27.00457°
Altitude
519.936 km
Speed
7.606 km/s
True Right ascension
08h 43m 11s
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
00:57:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
530.211 km
Perigee altitude
507.647 km
Semi-major axis
6,897.066 km
Eccentricity
0.00164
Inclination
97.5604°
RAAN
130.7967°
Arg. of periapsis
296.8475°
True anomaly
63.27573°
Mean anomaly
63.1084°
Eccentric anomaly
63.19205°
Mean motion
3.78919 °/min
Orbital period
95.01 mins
BSTAR
0.0002589
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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 | 2026-06-06 21:56:48.289Z | 135.099° SSE | 2026-06-06 21:59:48.289Z | 66.217° ENE | 30.484° | 2026-06-06 22:02:48.289Z | 7.527° NNE |
| 5 mins | 2026-06-07 11:04:48.289Z | 29.675° NE | 2026-06-07 11:06:48.289Z | 106.69° ESE | 40.593° | 2026-06-07 11:09:48.289Z | 178.625° S |
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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