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: 14 hours ago
TLE from 14 hours ago
0 SKYKRAFT-1
1 55041U 23001AJ 25340.64738387 .00049010 00000-0 88237-3 0 9996
2 55041 97.3487 47.2538 0006920 58.4142 301.7784 15.49641478163071Epoch: 2025-12-06T15:32Z
TLE epoch observation values (Epoch: 2025-12-06T15:32:13.966Z)
Latitude
-0.00001°
Longitude
98.52349°
Altitude
418.431 km
Speed
7.661 km/s
True Right ascension
03h 09m 00s
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
03:46:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
419.399 km
Perigee altitude
409.997 km
Semi-major axis
6,792.835 km
Eccentricity
0.00069
Inclination
97.3487°
RAAN
47.2538°
Arg. of periapsis
58.4142°
True anomaly
301.71096°
Mean anomaly
301.7784°
Eccentric anomaly
301.74468°
Mean motion
3.87674 °/min
Orbital period
92.86 mins
BSTAR
0.00088237
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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 | 2025-12-07 16:53:40.780Z | 39.964° NE | 2025-12-07 16:56:40.780Z | 110.595° ESE | 22.259° | 2025-12-07 16:58:40.780Z | 151.881° SSE |
| 4 mins | 2025-12-08 04:52:40.780Z | 192.066° SSW | 2025-12-08 04:53:40.780Z | 227.641° WSW | 38.476° | 2025-12-08 04:56:40.780Z | 337.916° N |
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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