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: 5 hours ago
TLE from 5 hours ago
0 LEMUR 2 NEUROSPICY
1 63355U 25061E 26099.24156996 .00003573 00000-0 20153-3 0 9996
2 63355 97.5584 75.4207 0018367 133.3310 226.9455 15.13681907 57181Epoch: 2026-04-09T05:47Z
TLE epoch observation values (Epoch: 2026-04-09T05:47:51.644Z)
Latitude
-0.00012°
Longitude
150.96313°
Altitude
536.731 km
Speed
7.589 km/s
True Right ascension
05h 01m 40s
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
17:24:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
534.637 km
Perigee altitude
509.29 km
Semi-major axis
6,900.101 km
Eccentricity
0.00184
Inclination
97.5584°
RAAN
75.4207°
Arg. of periapsis
133.331°
True anomaly
226.79195°
Mean anomaly
226.9455°
Eccentric anomaly
226.8687°
Mean motion
3.78669 °/min
Orbital period
95.07 mins
BSTAR
0.00020153
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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 | 2026-04-09 21:48:34.255Z | 124.793° SE | 2026-04-09 21:50:34.255Z | 82.82° E | 26.637° | 2026-04-09 21:53:34.255Z | 15.036° NNE |
| 5 mins | 2026-04-10 10:56:34.255Z | 37.44° NE | 2026-04-10 10:58:34.255Z | 112.249° ESE | 36.56° | 2026-04-10 11:01:34.255Z | 173.768° S |
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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