SKYCRAFT 4A, 64897
Orbit data source: Space-Track
SKYCRAFT 4A, 64897 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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64897 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: 16 hours ago
TLE from 16 hours ago
0 SKYCRAFT 4A
1 64897U 25154J 26225.18160314 .00002255 00000-0 19934-3 0 9995
2 64897 97.6664 288.5314 0006687 82.1277 278.0704 14.97307733 55911Epoch: 2026-08-13T04:21Z
TLE epoch observation values (Epoch: 2026-08-13T04:21:30.511Z)
Latitude
-0°
Longitude
-98.4706°
Altitude
577.621 km
Speed
7.572 km/s
True Right ascension
19h 14m 07s
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
11:11:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
576.874 km
Perigee altitude
567.579 km
Semi-major axis
6,950.363 km
Eccentricity
0.00067
Inclination
97.6664°
RAAN
288.5314°
Arg. of periapsis
82.1277°
True anomaly
277.99452°
Mean anomaly
278.0704°
Eccentric anomaly
278.03246°
Mean motion
3.74569 °/min
Orbital period
96.11 mins
BSTAR
0.00019934
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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 4A 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 | 2026-08-14 04:32:44.026Z | 181.794° SSW | 2026-08-14 04:35:44.026Z | 270.633° WNW | 41.194° | 2026-08-14 04:38:44.026Z | 337.89° N |
| 4 mins | 2026-08-14 16:14:44.026Z | 65.082° ENE | 2026-08-14 16:16:44.026Z | 102.201° ESE | 17.47° | 2026-08-14 16:18:44.026Z | 134.234° SE |
| 5 mins | 2026-08-14 17:49:44.026Z | 333.752° NNW | 2026-08-14 17:51:44.026Z | 284.246° WNW | 27.474° | 2026-08-14 17:54:44.026Z | 229.479° 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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