HUBBLE 6, 64562
Orbit data source: Space-Track
HUBBLE 6, 64562 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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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: 12 hours ago
TLE from 12 hours ago
0 HUBBLE 6
1 64562U 25135AL 26062.31123173 .00002951 00000-0 28970-3 0 9992
2 64562 97.7623 177.7807 0001317 119.2813 240.8538 14.92940783 38078Epoch: 2026-03-03T07:28Z
TLE epoch observation values (Epoch: 2026-03-03T07:28:10.421Z)
Latitude
-0.00004°
Longitude
-95.35483°
Altitude
592.262 km
Speed
7.564 km/s
True Right ascension
11h 51m 07s
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
23:39:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
586.706 km
Perigee altitude
584.872 km
Semi-major axis
6,963.926 km
Eccentricity
0.00013
Inclination
97.7623°
RAAN
177.7807°
Arg. of periapsis
119.2813°
True anomaly
240.84062°
Mean anomaly
240.8538°
Eccentric anomaly
240.84721°
Mean motion
3.73475 °/min
Orbital period
96.39 mins
BSTAR
0.0002897
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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 6 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-03-03 20:54:07.474Z | 356.389° N | 2026-03-03 20:57:07.474Z | 298.128° NW | 35.466° | 2026-03-03 21:01:07.474Z | 214.626° SW |
| 6 mins | 2026-03-04 07:44:07.474Z | 173.806° S | 2026-03-04 07:46:07.474Z | 197.898° SSW | 42.56° | 2026-03-04 07:50:07.474Z | 344.07° N |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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