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: 20 hours ago
TLE from 20 hours ago
0 SKYKRAFT-3D
1 57956U 23084BZ 26016.37161812 .00036696 00000-0 50834-3 0 9996
2 57956 97.5929 163.1057 0004200 100.7693 259.4035 15.56997490131389Epoch: 2026-01-16T08:55Z
TLE epoch observation values (Epoch: 2026-01-16T08:55:07.805Z)
Latitude
0.00002°
Longitude
-86.48868°
Altitude
400.012 km
Speed
7.67 km/s
True Right ascension
10h 52m 25s
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
05:19:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
396.121 km
Perigee altitude
390.433 km
Semi-major axis
6,771.414 km
Eccentricity
0.00042
Inclination
97.5929°
RAAN
163.1057°
Arg. of periapsis
100.7693°
True anomaly
259.3562°
Mean anomaly
259.4035°
Eccentric anomaly
259.37985°
Mean motion
3.89515 °/min
Orbital period
92.42 mins
BSTAR
0.00050834
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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 | 2026-01-17 09:43:13.288Z | 168.779° S | 2026-01-17 09:46:13.288Z | 296.103° NW | 44.778° | 2026-01-17 09:48:13.288Z | 345.66° N |
| 4 mins | 2026-01-17 22:30:13.288Z | 17.235° NNE | 2026-01-17 22:32:13.288Z | 146.446° SSE | 43.852° | 2026-01-17 22:34:13.288Z | 187.834° SSW |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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