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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64562 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: 12 hours ago
TLE from 12 hours ago
0 HUBBLE 6
1 64562U 25135AL 26224.59456261 .00000902 00000-0 90671-4 0 9991
2 64562 97.7791 338.1706 0001280 97.4199 262.7167 14.93668236 62291Epoch: 2026-08-12T14:16Z
TLE epoch observation values (Epoch: 2026-08-12T14:16:10.209Z)
Latitude
0.00005°
Longitude
163.0818°
Altitude
589.666 km
Speed
7.565 km/s
True Right ascension
22h 32m 40s
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
16:56:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
584.418 km
Perigee altitude
582.636 km
Semi-major axis
6,961.664 km
Eccentricity
0.00013
Inclination
97.7791°
RAAN
338.1706°
Arg. of periapsis
97.4199°
True anomaly
262.70215°
Mean anomaly
262.7167°
Eccentric anomaly
262.70943°
Mean motion
3.73657 °/min
Orbital period
96.34 mins
BSTAR
0.000090671
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-08-13 08:05:19.634Z | 197.07° SSW | 2026-08-13 08:08:19.634Z | 282.191° WNW | 33.831° | 2026-08-13 08:11:19.634Z | 331.912° NNW |
| 5 mins | 2026-08-13 19:48:19.634Z | 54.129° ENE | 2026-08-13 19:50:19.634Z | 95.951° ESE | 23.821° | 2026-08-13 19:53:19.634Z | 149.644° SSE |
| 4 mins | 2026-08-13 21:24:19.634Z | 319.351° NNW | 2026-08-13 21:25:19.634Z | 298.659° NW | 21.552° | 2026-08-13 21:28:19.634Z | 243.938° WSW |
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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