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, 14.5 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 NEUROSPICY
1 63355U 25061E 26154.43297257 .00004338 00000-0 24142-3 0 9997
2 63355 97.5616 130.2128 0015369 311.3082 48.6825 15.14088834 65531Epoch: 2026-06-03T10:23Z
TLE epoch observation values (Epoch: 2026-06-03T10:23:28.830Z)
Latitude
-0.00007°
Longitude
82.45102°
Altitude
519.828 km
Speed
7.607 km/s
True Right ascension
08h 40m 51s
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
00:51:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
531.329 km
Perigee altitude
510.124 km
Semi-major axis
6,898.864 km
Eccentricity
0.00154
Inclination
97.5616°
RAAN
130.2128°
Arg. of periapsis
311.3082°
True anomaly
48.81494°
Mean anomaly
48.6825°
Eccentric anomaly
48.7487°
Mean motion
3.78771 °/min
Orbital period
95.04 mins
BSTAR
0.00024142
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-06 22:34:47.506Z | 177.025° S | 2026-06-06 22:37:47.506Z | 257.873° W | 42.782° | 2026-06-06 22:40:47.506Z | 340.544° N |
| 6 mins | 2026-06-07 11:42:47.506Z | 348.87° N | 2026-06-07 11:44:47.506Z | 304.672° NW | 32.469° | 2026-06-07 11:48:47.506Z | 216.524° SW |
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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