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: 7 hours ago
TLE from 7 hours ago
0 LEMUR 2 NEUROSPICY
1 63355U 25061E 26279.17302546 .00002769 00000-0 15207-3 0 9992
2 63355 97.5765 254.2926 0015073 232.8723 127.1132 15.14885465 84417Epoch: 2026-10-06T04:09Z
TLE epoch observation values (Epoch: 2026-10-06T04:09:09.399Z)
Latitude
-0.00008°
Longitude
177.16208°
Altitude
530.691 km
Speed
7.594 km/s
True Right ascension
16h 57m 10s
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
05:27:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
528.701 km
Perigee altitude
507.911 km
Semi-major axis
6,896.443 km
Eccentricity
0.00151
Inclination
97.5765°
RAAN
254.2926°
Arg. of periapsis
232.8723°
True anomaly
127.25078°
Mean anomaly
127.1132°
Eccentric anomaly
127.18201°
Mean motion
3.78971 °/min
Orbital period
94.99 mins
BSTAR
0.00015207
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-10-06 21:44:43.121Z | 111.685° ESE | 2026-10-06 21:46:43.121Z | 70.252° E | 23.937° | 2026-10-06 21:49:43.121Z | 16.835° NNE |
| 4 mins | 2026-10-06 23:19:43.121Z | 240.255° WSW | 2026-10-06 23:20:43.121Z | 262.686° W | 22.186° | 2026-10-06 23:23:43.121Z | 316.048° NNW |
| 5 mins | 2026-10-07 10:51:43.121Z | 45.85° ENE | 2026-10-07 10:53:43.121Z | 101.641° ESE | 35.39° | 2026-10-07 10:56:43.121Z | 162.843° 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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