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: 19 hours ago
TLE from 19 hours ago
0 LEMUR 2 ESPERANZA
1 63352U 25061B 26042.34787122 .00006423 00000-0 37134-3 0 9997
2 63352 97.5517 18.8832 0018290 344.0598 16.0054 15.12487953 48562Epoch: 2026-02-11T08:20Z
TLE epoch observation values (Epoch: 2026-02-11T08:20:56.073Z)
Latitude
-0.00009°
Longitude
112.2343°
Altitude
519.548 km
Speed
7.61 km/s
True Right ascension
01h 15m 31s
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
05:52:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
538.225 km
Perigee altitude
512.971 km
Semi-major axis
6,903.735 km
Eccentricity
0.00183
Inclination
97.5517°
RAAN
18.8832°
Arg. of periapsis
344.0598°
True anomaly
16.06332°
Mean anomaly
16.0054°
Eccentric anomaly
16.03435°
Mean motion
3.7837 °/min
Orbital period
95.14 mins
BSTAR
0.00037134
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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 | 2026-02-12 10:20:29.852Z | 56.556° ENE | 2026-02-12 10:22:29.852Z | 93.506° ESE | 18.477° | 2026-02-12 10:24:29.852Z | 131.029° SE |
| 4 mins | 2026-02-12 11:55:29.852Z | 322.74° NNW | 2026-02-12 11:56:29.852Z | 298.53° NW | 24.461° | 2026-02-12 11:59:29.852Z | 236.243° WSW |
| 6 mins | 2026-02-12 22:35:29.852Z | 184.265° SSW | 2026-02-12 22:37:29.852Z | 232.661° WSW | 40.139° | 2026-02-12 22:41:29.852Z | 340.315° N |
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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