LEMUR 2 ESPERANZA, 63352
Orbit data source: Space-Track
LEMUR 2 ESPERANZA, 63352 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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63352 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: 10 hours ago
TLE from 10 hours ago
0 LEMUR 2 ESPERANZA
1 63352U 25061B 26049.42660210 .00004466 00000-0 25898-3 0 9990
2 63352 97.5530 25.8868 0017522 318.6937 41.2967 15.12557109 49638Epoch: 2026-02-18T10:14Z
TLE epoch observation values (Epoch: 2026-02-18T10:14:18.421Z)
Latitude
-0.00005°
Longitude
83.91764°
Altitude
522.396 km
Speed
7.607 km/s
True Right ascension
01h 43m 32s
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
23:03:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
537.483 km
Perigee altitude
513.291 km
Semi-major axis
6,903.524 km
Eccentricity
0.00175
Inclination
97.553°
RAAN
25.8868°
Arg. of periapsis
318.6937°
True anomaly
41.42943°
Mean anomaly
41.2967°
Eccentric anomaly
41.36304°
Mean motion
3.78388 °/min
Orbital period
95.14 mins
BSTAR
0.00025898
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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 ESPERANZA 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 | 2026-02-18 21:30:02.057Z | 113.485° SE | 2026-02-18 21:33:02.057Z | 57.946° ENE | 18.581° | 2026-02-18 21:35:02.057Z | 24.385° NE |
| 4 mins | 2026-02-18 23:05:02.057Z | 225.039° WSW | 2026-02-18 23:07:02.057Z | 273.342° WNW | 23.254° | 2026-02-18 23:09:02.057Z | 312.839° NW |
| 4 mins | 2026-02-19 10:39:02.057Z | 56.737° ENE | 2026-02-19 10:40:02.057Z | 81.525° E | 26.711° | 2026-02-19 10:43:02.057Z | 152.482° SSE |
| 4 mins | 2026-02-19 12:13:02.057Z | 320.866° NNW | 2026-02-19 12:15:02.057Z | 283.264° WNW | 16.618° | 2026-02-19 12:17:02.057Z | 251.465° W |
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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