DRAGON ENDEAVOUR 6, 65077 (Decayed)
Orbit data source: Space-Track
DRAGON ENDEAVOUR 6, 65077 was 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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Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX
Mission
Decayed 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: 5 months ago
TLE from 5 months ago
0 DRAGON ENDEAVOUR 6
1 65077U 25166A 26032.11330074 .00006524 00000-0 12933-3 0 9995
2 65077 51.6318 253.1662 0011128 51.9836 308.2155 15.48314896 2141Epoch: 2026-02-01T02:43Z
TLE epoch observation values (Epoch: 2026-02-01T02:43:09.183Z)
Latitude
-0.00005°
Longitude
81.0503°
Altitude
417.72 km
Speed
7.664 km/s
True Right ascension
16h 52m 39s
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
07:19:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
429.732 km
Perigee altitude
414.597 km
Semi-major axis
6,800.301 km
Eccentricity
0.00111
Inclination
51.6318°
RAAN
253.1662°
Arg. of periapsis
51.9836°
True anomaly
308.11522°
Mean anomaly
308.2155°
Eccentric anomaly
308.16537°
Mean motion
3.87036 °/min
Orbital period
93.01 mins
BSTAR
0.00012933
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Other satellites on launch #166 in the year 2025 (2025-08-01 UTC)
No other RSOs were in this launch
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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.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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-21 09:53:26.438Z | 213.094° SW | 2026-06-21 09:56:26.438Z | 134.792° SE | 37.454° | 2026-06-21 09:59:26.438Z | 62.881° ENE |
| 4 mins | 2026-06-21 16:24:26.438Z | 322.321° NNW | 2026-06-21 16:26:26.438Z | 71.669° E | 39.316° | 2026-06-21 16:28:26.438Z | 113.021° SE |
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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