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, 14.5 m
Radar Cross Section
0.065 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 SKYCRAFT 4E
1 65227U 25154L 26149.14805556 .00007911 00000-0 68088-3 0 9996
2 65227 97.6708 214.2770 0004081 343.7254 16.3836 14.97628001 44480Epoch: 2026-05-29T03:33Z
TLE epoch observation values (Epoch: 2026-05-29T03:33:12.000Z)
Latitude
-0.00007°
Longitude
-85.70559°
Altitude
574.557 km
Speed
7.575 km/s
True Right ascension
14h 17m 06s
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
01:47:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
574.071 km
Perigee altitude
568.399 km
Semi-major axis
6,949.372 km
Eccentricity
0.00041
Inclination
97.6708°
RAAN
214.277°
Arg. of periapsis
343.7254°
True anomaly
16.3968°
Mean anomaly
16.3836°
Eccentric anomaly
16.3902°
Mean motion
3.74649 °/min
Orbital period
96.09 mins
BSTAR
0.00068088
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-05-29 16:56:22.109Z | 21.005° NNE | 2026-05-29 17:00:22.109Z | 101.605° ESE | 39.826° | 2026-05-29 17:03:22.109Z | 175.735° S |
| 5 mins | 2026-05-30 03:45:22.109Z | 122.014° SE | 2026-05-30 03:47:22.109Z | 79.426° E | 27.498° | 2026-05-30 03:50:22.109Z | 15.162° NNE |
| 4 mins | 2026-05-30 05:21:22.109Z | 238.382° WSW | 2026-05-30 05:23:22.109Z | 275.52° WNW | 17.275° | 2026-05-30 05:25:22.109Z | 307.079° NW |
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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