SKYCRAFT 4C, 64896
Orbit data source: Space-Track
SKYCRAFT 4C, 64896 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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64896 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 4C
1 64896U 25154H 26270.12018624 .00002200 00000-0 20297-3 0 9998
2 64896 97.6588 332.0141 0003805 280.6491 79.4302 14.95647631214387Epoch: 2026-09-27T02:53Z
TLE epoch observation values (Epoch: 2026-09-27T02:53:04.091Z)
Latitude
0.00004°
Longitude
-77.17141°
Altitude
582.928 km
Speed
7.569 km/s
True Right ascension
22h 08m 03s
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
21:46:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
580.019 km
Perigee altitude
574.726 km
Semi-major axis
6,955.51 km
Eccentricity
0.00038
Inclination
97.6588°
RAAN
332.0141°
Arg. of periapsis
280.6491°
True anomaly
79.47307°
Mean anomaly
79.4302°
Eccentric anomaly
79.45163°
Mean motion
3.74153 °/min
Orbital period
96.22 mins
BSTAR
0.00020297
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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 4C 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 | 2026-09-28 04:41:49.763Z | 192.95° SSW | 2026-09-28 04:44:49.763Z | 254.36° W | 42.987° | 2026-09-28 04:48:49.763Z | 333.447° NNW |
| 5 mins | 2026-09-28 16:24:49.763Z | 56.761° ENE | 2026-09-28 16:26:49.763Z | 101.414° ESE | 26.698° | 2026-09-28 16:29:49.763Z | 152.13° SSE |
| 5 mins | 2026-09-28 17:59:49.763Z | 329.455° NNW | 2026-09-28 18:01:49.763Z | 290.878° WNW | 23.051° | 2026-09-28 18:04:49.763Z | 241.018° WSW |
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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