SKYCRAFT 4E, 65227
Orbit data source: Space-Track
SKYCRAFT 4E, 65227 is a payload satellite owned by SkyKraft (AU) in SSO that was launched on Wed, 23 Jul 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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65227 intel report (Beta)
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Identifier
Orbit
Country
AU / AUSRelated business
Manufacturer
SkyKraft
Mission
Operational Commercial Communications
Bus & Motor
SKYKRAFT, Unknown motor
Mass
~50 kg wet, ~50 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.3 m
Radar Cross Section
0.065 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 SKYCRAFT 4E
1 65227U 25154L 26269.75392979 .00004346 00000-0 36362-3 0 9995
2 65227 97.6596 332.7847 0004028 289.7132 70.3656 14.98977165 62547Epoch: 2026-09-26T18:05Z
TLE epoch observation values (Epoch: 2026-09-26T18:05:39.533Z)
Latitude
-0.00007°
Longitude
55.81253°
Altitude
572.17 km
Speed
7.575 km/s
True Right ascension
22h 11m 08s
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
21:49:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
569.858 km
Perigee altitude
564.263 km
Semi-major axis
6,945.197 km
Eccentricity
0.0004
Inclination
97.6596°
RAAN
332.7847°
Arg. of periapsis
289.7132°
True anomaly
70.40908°
Mean anomaly
70.3656°
Eccentric anomaly
70.38734°
Mean motion
3.74987 °/min
Orbital period
96 mins
BSTAR
0.00036362
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Other satellites on launch #154 in the year 2025 (2025-07-23 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.SKYCRAFT 4E 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 | 2026-09-28 05:28:55.991Z | 240.198° WSW | 2026-09-28 05:30:55.991Z | 272.17° WNW | 14.581° | 2026-09-28 05:32:55.991Z | 301.946° NW |
| 6 mins | 2026-09-28 17:07:55.991Z | 16.358° NNE | 2026-09-28 17:10:55.991Z | 156.179° SSE | 73.248° | 2026-09-28 17:13:55.991Z | 188.855° SSW |
| 6 mins | 2026-09-29 03:54:55.991Z | 132.969° SE | 2026-09-29 03:56:55.991Z | 85.141° E | 41.742° | 2026-09-29 04:00:55.991Z | 2.588° NNE |
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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