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 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 ESPERANZA
1 63352U 25061B 26154.44656555 .00003752 00000-0 21282-3 0 9996
2 63352 97.5640 130.0007 0017039 316.2764 43.7116 15.13467094 65511Epoch: 2026-06-03T10:43Z
TLE epoch observation values (Epoch: 2026-06-03T10:43:03.263Z)
Latitude
-0.00009°
Longitude
77.33205°
Altitude
520.218 km
Speed
7.608 km/s
True Right ascension
08h 40m 00s
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
00:54:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
534.376 km
Perigee altitude
510.859 km
Semi-major axis
6,900.755 km
Eccentricity
0.0017
Inclination
97.564°
RAAN
130.0007°
Arg. of periapsis
316.2764°
True anomaly
43.84673°
Mean anomaly
43.7116°
Eccentric anomaly
43.77915°
Mean motion
3.78615 °/min
Orbital period
95.08 mins
BSTAR
0.00021282
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-06 21:23:11.700Z | 102.331° ESE | 2026-06-06 21:25:11.700Z | 69.233° E | 15.188° | 2026-06-06 21:27:11.700Z | 34.845° NE |
| 5 mins | 2026-06-06 22:57:11.700Z | 209.316° SW | 2026-06-06 22:59:11.700Z | 259.878° W | 29.145° | 2026-06-06 23:02:11.700Z | 324.648° NNW |
| 4 mins | 2026-06-07 10:31:11.700Z | 62.284° ENE | 2026-06-07 10:32:11.700Z | 83.468° E | 21.321° | 2026-06-07 10:35:11.700Z | 143.759° SSE |
| 4 mins | 2026-06-07 12:05:11.700Z | 325.02° NNW | 2026-06-07 12:07:11.700Z | 281.339° WNW | 20.78° | 2026-06-07 12:09:11.700Z | 245.222° WSW |
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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