HUBBLE 7, 64592
Orbit data source: Space-Track
HUBBLE 7, 64592 is an American payload satellite in SSO that was launched on Mon, 23 Jun 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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64592 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Endurosat
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 16U, Unknown motor
Mass
22 kg wet, 22 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 4 Pan, 1.0 m
Radar Cross Section
0.326 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 HUBBLE 7
1 64592U 25135BS 26119.85617487 .00004601 00000-0 44043-3 0 9996
2 64592 97.7677 235.0767 0004544 151.2826 208.8645 14.93670351 46690Epoch: 2026-04-29T20:32Z
TLE epoch observation values (Epoch: 2026-04-29T20:32:53.508Z)
Latitude
-0.00001°
Longitude
69.04262°
Altitude
592.319 km
Speed
7.562 km/s
True Right ascension
15h 40m 18s
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
19:56:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
586.683 km
Perigee altitude
580.356 km
Semi-major axis
6,961.657 km
Eccentricity
0.00045
Inclination
97.7677°
RAAN
235.0767°
Arg. of periapsis
151.2826°
True anomaly
208.83938°
Mean anomaly
208.8645°
Eccentric anomaly
208.85194°
Mean motion
3.73658 °/min
Orbital period
96.34 mins
BSTAR
0.00044043
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Other satellites on launch #135 in the year 2025 (2025-06-23 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.HUBBLE 7 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-04-30 19:38:13.988Z | 46.278° ENE | 2026-04-30 19:41:13.988Z | 94.595° ESE | 19.312° | 2026-04-30 19:44:13.988Z | 142.745° SSE |
| 5 mins | 2026-04-30 21:14:13.988Z | 340.018° N | 2026-04-30 21:16:13.988Z | 301.96° NW | 25.668° | 2026-04-30 21:19:13.988Z | 237.909° WSW |
| 6 mins | 2026-05-01 08:03:13.988Z | 194.394° SSW | 2026-05-01 08:05:13.988Z | 237.496° WSW | 35.44° | 2026-05-01 08:09:13.988Z | 333.673° NNW |
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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