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: 8 hours ago
TLE from 8 hours ago
0 HUBBLE 7
1 64592U 25135BS 26132.04884500 .00001271 00000-0 12580-3 0 9995
2 64592 97.7711 247.1345 0004307 103.6326 256.5374 14.93610764 48512Epoch: 2026-05-12T01:10Z
TLE epoch observation values (Epoch: 2026-05-12T01:10:20.207Z)
Latitude
0.00005°
Longitude
-0.27851°
Altitude
590.432 km
Speed
7.564 km/s
True Right ascension
16h 28m 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
17:46:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
586.704 km
Perigee altitude
580.707 km
Semi-major axis
6,961.842 km
Eccentricity
0.00043
Inclination
97.7711°
RAAN
247.1345°
Arg. of periapsis
103.6326°
True anomaly
256.48941°
Mean anomaly
256.5374°
Eccentric anomaly
256.5134°
Mean motion
3.73643 °/min
Orbital period
96.35 mins
BSTAR
0.0001258
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-05-12 19:27:33.791Z | 64.357° ENE | 2026-05-12 19:29:33.791Z | 96.35° ESE | 14.595° | 2026-05-12 19:31:33.791Z | 126.475° SE |
| 6 mins | 2026-05-12 21:02:33.791Z | 346.453° N | 2026-05-12 21:04:33.791Z | 302.713° NW | 32.1° | 2026-05-12 21:08:33.791Z | 219.541° SW |
| 6 mins | 2026-05-13 07:51:33.791Z | 180.57° SSW | 2026-05-13 07:53:33.791Z | 222.796° SW | 41.716° | 2026-05-13 07:57:33.791Z | 341.203° 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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