DRAGON ENDURANCE 4, 63204 (Decayed)
Orbit data source: Space-Track
DRAGON ENDURANCE 4, 63204 was a payload satellite owned by SpaceX (US) in LEO that was launched on Fri, 14 Mar 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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63204 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, 2.6 m
Radar Cross Section
21.677 m²
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 DRAGON ENDURANCE 4
1 63204U 25049A 25222.92732718 .00008419 00000-0 15293-3 0 9992
2 63204 51.6346 35.7476 0001307 177.0594 183.0403 15.50446935 22890Epoch: 2025-08-10T22:15Z
TLE epoch observation values (Epoch: 2025-08-10T22:15:21.068Z)
Latitude
-0.00001°
Longitude
102.26816°
Altitude
417.048 km
Speed
7.662 km/s
True Right ascension
02h 22m 59s
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
02:20:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
416.817 km
Perigee altitude
415.041 km
Semi-major axis
6,794.066 km
Eccentricity
0.00013
Inclination
51.6346°
RAAN
35.7476°
Arg. of periapsis
177.0594°
True anomaly
183.03951°
Mean anomaly
183.0403°
Eccentric anomaly
183.0399°
Mean motion
3.87569 °/min
Orbital period
92.89 mins
BSTAR
0.00015293
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Other satellites on launch #49 in the year 2025 (2025-03-14 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 ENDURANCE 4 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 | 2026-11-02 10:24:48.464Z | 317.608° NNW | 2026-11-02 10:26:48.464Z | 65.296° ENE | 63.129° | 2026-11-02 10:28:48.464Z | 116.224° SE |
| 4 mins | 2026-11-03 04:36:48.464Z | 286.873° WNW | 2026-11-03 04:37:48.464Z | 321.091° NNW | 32.542° | 2026-11-03 04:40:48.464Z | 36.245° NE |
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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