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: 13 hours ago
TLE from 13 hours ago
0 HUBBLE 6
1 64562U 25135AL 26131.88125524 .00001028 00000-0 10240-3 0 9998
2 64562 97.7708 246.4517 0001349 104.8705 255.2664 14.93752034 48453Epoch: 2026-05-11T21:09Z
TLE epoch observation values (Epoch: 2026-05-11T21:09:00.452Z)
Latitude
-0.00007°
Longitude
59.5362°
Altitude
589.532 km
Speed
7.565 km/s
True Right ascension
16h 25m 48s
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
18:24:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
584.205 km
Perigee altitude
582.327 km
Semi-major axis
6,961.403 km
Eccentricity
0.00013
Inclination
97.7708°
RAAN
246.4517°
Arg. of periapsis
104.8705°
True anomaly
255.25145°
Mean anomaly
255.2664°
Eccentric anomaly
255.25893°
Mean motion
3.73678 °/min
Orbital period
96.34 mins
BSTAR
0.0001024
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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 | 2026-05-12 20:13:13.612Z | 22.045° NNE | 2026-05-12 20:17:13.612Z | 114.448° SE | 39.414° | 2026-05-12 20:20:13.612Z | 176.301° S |
| 5 mins | 2026-05-13 07:04:13.612Z | 116.049° SE | 2026-05-13 07:06:13.612Z | 62.975° ENE | 28.911° | 2026-05-13 07:09:13.612Z | 9.69° NNE |
| 4 mins | 2026-05-13 08:40:13.612Z | 243.695° WSW | 2026-05-13 08:41:13.612Z | 261.516° W | 17.039° | 2026-05-13 08:44:13.612Z | 309.179° NW |
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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