SKYKRAFT-1, 55041
Orbit data source: Space-Track
SKYKRAFT-1, 55041 is a payload satellite owned by SkyKraft (AU) in SSO that was launched on Tue, 03 Jan 2023 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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55041 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
AU / AUSRelated business
Manufacturer
SkyKraft
Mission
Operational Commercial Technology
Bus & Motor
SKYKRAFT CARRIER, AOCS
Mass
~100 kg wet, ~100 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: 15 hours ago
TLE from 15 hours ago
0 SKYKRAFT-1
1 55041U 23001AJ 26022.47058743 .00044877 00000-0 70377-3 0 9998
2 55041 97.3384 95.0634 0004778 240.0727 120.0052 15.53557239170335Epoch: 2026-01-22T11:17Z
TLE epoch observation values (Epoch: 2026-01-22T11:17:38.753Z)
Latitude
-0.00008°
Longitude
163.82865°
Altitude
411.11 km
Speed
7.663 km/s
True Right ascension
06h 20m 15s
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
03:47:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
406.508 km
Perigee altitude
400.028 km
Semi-major axis
6,781.405 km
Eccentricity
0.00048
Inclination
97.3384°
RAAN
95.0634°
Arg. of periapsis
240.0727°
True anomaly
120.0526°
Mean anomaly
120.0052°
Eccentric anomaly
120.0289°
Mean motion
3.88654 °/min
Orbital period
92.63 mins
BSTAR
0.00070377
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Other satellites on launch #1 in the year 2023 (2023-01-03 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-1 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 | 2026-01-23 04:25:37.556Z | 145.415° SSE | 2026-01-23 04:28:37.556Z | 66.917° ENE | 33.155° | 2026-01-23 04:30:37.556Z | 9.235° NNE |
| 4 mins | 2026-01-23 17:14:37.556Z | 45.796° ENE | 2026-01-23 17:15:37.556Z | 77.459° E | 30.273° | 2026-01-23 17:18:37.556Z | 166.662° 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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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