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 6U, Unknown motor
Mass
~15 kg wet, ~15 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 14.5 m
Radar Cross Section
0.065 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 LEMUR 2 NEUROSPICY
1 63355U 25061E 26042.37884693 .00005426 00000-0 30959-3 0 9994
2 63355 97.5499 19.0658 0016590 340.5340 19.5255 15.13058398 48581Epoch: 2026-02-11T09:05Z
TLE epoch observation values (Epoch: 2026-02-11T09:05:32.374Z)
Latitude
-0.00008°
Longitude
101.23511°
Altitude
519.159 km
Speed
7.61 km/s
True Right ascension
01h 16m 15s
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
05:53:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
535.311 km
Perigee altitude
512.41 km
Semi-major axis
6,901.998 km
Eccentricity
0.00166
Inclination
97.5499°
RAAN
19.0658°
Arg. of periapsis
340.534°
True anomaly
19.58916°
Mean anomaly
19.5255°
Eccentric anomaly
19.55732°
Mean motion
3.78513 °/min
Orbital period
95.11 mins
BSTAR
0.00030959
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-02-12 11:02:50.175Z | 18.742° NNE | 2026-02-12 11:05:50.175Z | 60.81° ENE | 40.991° | 2026-02-12 11:09:50.175Z | 183.738° SSW |
| 5 mins | 2026-02-12 21:44:50.175Z | 120.051° SE | 2026-02-12 21:46:50.175Z | 75.988° E | 25.365° | 2026-02-12 21:49:50.175Z | 14.663° NNE |
| 4 mins | 2026-02-12 23:19:50.175Z | 238.276° WSW | 2026-02-12 23:20:50.175Z | 256.823° W | 16.528° | 2026-02-12 23:23:50.175Z | 309.2° NW |
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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