DRAGON ENDEAVOUR 6, 65077
Orbit data source: Space-Track
DRAGON ENDEAVOUR 6, 65077 is a payload satellite owned by SpaceX (US) in LEO that was launched on Fri, 01 Aug 2025 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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65077 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX
Mission
Operational Commercial Spaceship
Bus & Motor
DRAGON CM, Unknown motor
Mass
~13,055 kg wet, ~9,500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Trunc Cone + Cyl + 4 Fin, 14.5 m
Radar Cross Section
21.677 m²
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 DRAGON ENDEAVOUR 6
1 65077U 25166A 25342.54239145 .00012445 00000-0 23028-3 0 9998
2 65077 51.6307 163.2617 0003394 220.7658 139.3077 15.49420853 2142Epoch: 2025-12-08T13:01Z
TLE epoch observation values (Epoch: 2025-12-08T13:01:02.621Z)
Latitude
-0.00001°
Longitude
-109.53916°
Altitude
420.909 km
Speed
7.659 km/s
True Right ascension
10h 53m 02s
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
21:51:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
421.235 km
Perigee altitude
416.622 km
Semi-major axis
6,797.066 km
Eccentricity
0.00034
Inclination
51.6307°
RAAN
163.2617°
Arg. of periapsis
220.7658°
True anomaly
139.33305°
Mean anomaly
139.3077°
Eccentric anomaly
139.32038°
Mean motion
3.87312 °/min
Orbital period
92.95 mins
BSTAR
0.00023028
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Other satellites on launch #166 in the year 2025 (2025-08-01 UTC)
No other RSOs were in this launch
Did you know?
You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.DRAGON ENDEAVOUR 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-12-09 13:56:46.917Z | 174.944° S | 2025-12-09 13:58:46.917Z | 133.196° SE | 18.704° | 2025-12-09 14:00:46.917Z | 90.367° ESE |
| 4 mins | 2025-12-09 15:33:46.917Z | 267.501° W | 2025-12-09 15:35:46.917Z | 350.069° N | 33.972° | 2025-12-09 15:37:46.917Z | 36.991° NE |
| 4 mins | 2025-12-09 20:26:46.917Z | 341.233° N | 2025-12-09 20:28:46.917Z | 41.54° NE | 25.389° | 2025-12-09 20:30:46.917Z | 84.945° E |
| 4 mins | 2025-12-09 22:03:46.917Z | 271.613° WNW | 2025-12-09 22:04:46.917Z | 241.944° WSW | 28.544° | 2025-12-09 22:07:46.917Z | 161.004° S |
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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