SKYKRAFT-3D, 57956
Orbit data source: Space-Track
SKYKRAFT-3D, 57956 is a payload satellite owned by SkyKraft (AU) in SSO that was launched on Mon, 12 Jun 2023 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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57956 intel report (Beta)
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Edit Public Description
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: 16 hours ago
TLE from 16 hours ago
0 SKYKRAFT-3D
1 57956U 23084BZ 25286.35435442 .00047987 00000-0 92161-3 0 9999
2 57956 97.5894 62.6868 0005924 90.7035 269.4893 15.47798086116640Epoch: 2025-10-13T08:30Z
TLE epoch observation values (Epoch: 2025-10-13T08:30:16.221Z)
Latitude
-0.0001°
Longitude
-87.03911°
Altitude
426.33 km
Speed
7.656 km/s
True Right ascension
04h 10m 44s
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
19:17:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
424.133 km
Perigee altitude
416.078 km
Semi-major axis
6,798.243 km
Eccentricity
0.00059
Inclination
97.5894°
RAAN
62.6868°
Arg. of periapsis
90.7035°
True anomaly
269.42142°
Mean anomaly
269.4893°
Eccentric anomaly
269.45536°
Mean motion
3.87211 °/min
Orbital period
92.97 mins
BSTAR
0.00092161
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Other satellites on launch #84 in the year 2023 (2023-06-12 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.SKYKRAFT-3D 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-14 09:27:38.175Z | 183.341° SSW | 2025-10-14 09:29:38.175Z | 227.006° WSW | 37.727° | 2025-10-14 09:32:38.175Z | 336.591° NNW |
| 4 mins | 2025-10-14 22:18:38.175Z | 356.216° N | 2025-10-14 22:20:38.175Z | 260.286° W | 39.319° | 2025-10-14 22:22:38.175Z | 208.989° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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