LEMUR 2 NEUROSPICY, 63355
Orbit data source: Space-Track
LEMUR 2 NEUROSPICY, 63355 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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63355 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: 10 hours ago
TLE from 10 hours ago
0 LEMUR 2 NEUROSPICY
1 63355U 25061E 26265.16935812 .00002553 00000-0 14079-3 0 9991
2 63355 97.5740 240.3423 0014896 286.8818 73.0780 15.14808331 82293Epoch: 2026-09-22T04:03Z
TLE epoch observation values (Epoch: 2026-09-22T04:03:52.541Z)
Latitude
-0.00005°
Longitude
178.33469°
Altitude
521.661 km
Speed
7.604 km/s
True Right ascension
16h 01m 22s
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
06:48:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
528.814 km
Perigee altitude
508.267 km
Semi-major axis
6,896.678 km
Eccentricity
0.00149
Inclination
97.574°
RAAN
240.3423°
Arg. of periapsis
286.8818°
True anomaly
73.24139°
Mean anomaly
73.078°
Eccentric anomaly
73.15969°
Mean motion
3.78951 °/min
Orbital period
95 mins
BSTAR
0.00014079
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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 NEUROSPICY 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-09-22 21:39:37.776Z | 107.195° ESE | 2026-09-22 21:41:37.776Z | 67.528° E | 21.137° | 2026-09-22 21:43:37.776Z | 29.07° NE |
| 5 mins | 2026-09-22 23:13:37.776Z | 221.601° SW | 2026-09-22 23:15:37.776Z | 265.319° W | 24.844° | 2026-09-22 23:18:37.776Z | 319.494° NNW |
| 5 mins | 2026-09-23 10:46:37.776Z | 50.421° ENE | 2026-09-23 10:48:37.776Z | 102.98° ESE | 31.401° | 2026-09-23 10:51:37.776Z | 159.385° 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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