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, 0.4 m
Radar Cross Section
0.065 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 LEMUR 2 TILLINFINITY
1 63356U 25061F 25309.64915622 .00005397 00000-0 31375-3 0 9997
2 63356 97.5367 282.6269 0017316 303.2304 56.7266 15.12380085 33821Epoch: 2025-11-05T15:34Z
TLE epoch observation values (Epoch: 2025-11-05T15:34:47.097Z)
Latitude
-0.00005°
Longitude
3.81187°
Altitude
525.471 km
Speed
7.604 km/s
True Right ascension
18h 50m 30s
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
04:08:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
537.881 km
Perigee altitude
513.97 km
Semi-major axis
6,904.062 km
Eccentricity
0.00173
Inclination
97.5367°
RAAN
282.6269°
Arg. of periapsis
303.2304°
True anomaly
56.89269°
Mean anomaly
56.7266°
Eccentric anomaly
56.80963°
Mean motion
3.78343 °/min
Orbital period
95.15 mins
BSTAR
0.00031375
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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 | 2025-11-06 11:11:29.446Z | 12.555° NNE | 2025-11-06 11:15:29.446Z | 187.207° SSW | 43.288° | 2025-11-06 11:18:29.446Z | 192.408° SSW |
| 5 mins | 2025-11-06 21:54:29.446Z | 119.292° SE | 2025-11-06 21:56:29.446Z | 54.03° ENE | 30.225° | 2025-11-06 21:59:29.446Z | 5.164° NNE |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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