HYDRA-T, 62692 (Decayed)
Orbit data source: Space-Track
HYDRA-T, 62692 was a Spanish payload satellite in LEO that was launched on Tue, 14 Jan 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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62692 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 2 months ago
TLE from 2 months ago
0 HYDRA-T
1 62692U 25009CM 26028.19742799 .10589489 24473-5 20739-2 0 9999
2 62692 97.3569 119.0624 0010828 297.3030 62.7162 16.31546071 58115Epoch: 2026-01-28T04:44Z
TLE epoch observation values (Epoch: 2026-01-28T04:44:17.778Z)
Latitude
-0.00001°
Longitude
-79.47961°
Altitude
188.376 km
Speed
7.795 km/s
True Right ascension
07h 56m 14s
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
15:55:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
192.312 km
Perigee altitude
178.098 km
Semi-major axis
6,563.342 km
Eccentricity
0.00108
Inclination
97.3569°
RAAN
119.0624°
Arg. of periapsis
297.303°
True anomaly
62.82654°
Mean anomaly
62.7162°
Eccentric anomaly
62.77137°
Mean motion
4.08184 °/min
Orbital period
88.2 mins
BSTAR
0.0020739
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Other satellites on launch #9 in the year 2025 (2025-01-14 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.HYDRA-T Visibility
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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. |
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| This satellite is decayed. |
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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