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: 20 hours ago
TLE from 20 hours ago
0 SKYCRAFT 4E
1 65227U 25154L 26318.20933089 .00005410 00000-0 44505-3 0 9994
2 65227 97.6552 20.3884 0006810 103.7287 256.4694 14.99511937 69804Epoch: 2026-11-14T05:01Z
TLE epoch observation values (Epoch: 2026-11-14T05:01:26.188Z)
Latitude
-0.00012°
Longitude
-108.2881°
Altitude
572.569 km
Speed
7.574 km/s
True Right ascension
01h 21m 33s
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
21:49:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
570.136 km
Perigee altitude
560.679 km
Semi-major axis
6,943.544 km
Eccentricity
0.00068
Inclination
97.6552°
RAAN
20.3884°
Arg. of periapsis
103.7287°
True anomaly
256.39354°
Mean anomaly
256.4694°
Eccentric anomaly
256.43147°
Mean motion
3.75121 °/min
Orbital period
95.97 mins
BSTAR
0.00044505
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-11-15 03:34:57.331Z | 124.595° SE | 2026-11-15 03:37:57.331Z | 72.899° E | 26.075° | 2026-11-15 03:40:57.331Z | 17.322° NNE |
| 5 mins | 2026-11-15 05:10:57.331Z | 224.066° SW | 2026-11-15 05:12:57.331Z | 261.488° W | 22.317° | 2026-11-15 05:15:57.331Z | 314.164° NW |
| 6 mins | 2026-11-15 16:49:57.331Z | 29.084° NE | 2026-11-15 16:52:57.331Z | 103.593° ESE | 47.976° | 2026-11-15 16:55:57.331Z | 170.754° 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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