SKYKRAFT-1C, 55061
Orbit data source: Space-Track
SKYKRAFT-1C, 55061 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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55061 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: 2 days ago
TLE from 2 days ago
0 SKYKRAFT-1C
1 55061U 23001BE 25312.41900334 .00005813 00000-0 24876-3 0 9997
2 55061 97.3535 5.7882 0010370 196.4262 163.6641 15.23144459157853Epoch: 2025-11-08T10:03Z
TLE epoch observation values (Epoch: 2025-11-08T10:03:21.888Z)
Latitude
0.00003°
Longitude
167.09811°
Altitude
506.302 km
Speed
7.607 km/s
True Right ascension
00h 23m 09s
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
19:04:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
500.448 km
Perigee altitude
486.197 km
Semi-major axis
6,871.459 km
Eccentricity
0.00104
Inclination
97.3535°
RAAN
5.7882°
Arg. of periapsis
196.4262°
True anomaly
163.69748°
Mean anomaly
163.6641°
Eccentric anomaly
163.6808°
Mean motion
3.81039 °/min
Orbital period
94.48 mins
BSTAR
0.00024876
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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-1C 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 | 2025-11-10 03:10:51.516Z | 134.907° SE | 2025-11-10 03:13:51.516Z | 78.002° E | 27.556° | 2025-11-10 03:16:51.516Z | 12.186° NNE |
| 5 mins | 2025-11-10 16:14:51.516Z | 37.306° NE | 2025-11-10 16:16:51.516Z | 108.213° ESE | 35.57° | 2025-11-10 16:19:51.516Z | 172.368° S |
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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