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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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, 14.5 m
Radar Cross Section
0.065 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 LEMUR 2 NEUROSPICY
1 63355U 25061E 25309.85979012 .00005343 00000-0 31536-3 0 9992
2 63355 97.5383 282.6985 0016311 315.1361 44.8550 15.11844181 33849Epoch: 2025-11-05T20:38Z
TLE epoch observation values (Epoch: 2025-11-05T20:38:05.866Z)
Latitude
-0.00001°
Longitude
-72.15235°
Altitude
525.67 km
Speed
7.605 km/s
True Right ascension
18h 50m 47s
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
538.822 km
Perigee altitude
516.295 km
Semi-major axis
6,905.695 km
Eccentricity
0.00163
Inclination
97.5383°
RAAN
282.6985°
Arg. of periapsis
315.1361°
True anomaly
44.98702°
Mean anomaly
44.855°
Eccentric anomaly
44.92099°
Mean motion
3.78209 °/min
Orbital period
95.19 mins
BSTAR
0.00031536
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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 | 2025-11-06 11:29:29.188Z | 359.947° N | 2025-11-06 11:32:29.188Z | 295.536° NW | 38.629° | 2025-11-06 11:35:29.188Z | 212.399° SW |
| 6 mins | 2025-11-06 22:11:29.188Z | 152.259° SSE | 2025-11-06 22:13:29.188Z | 104.567° ESE | 41.4° | 2025-11-06 22:17:29.188Z | 354.292° N |
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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