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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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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 SKYKRAFT-1C
1 55061U 23001BE 26166.10465015 .00003109 00000-0 12731-3 0 9996
2 55061 97.3195 219.8064 0011418 146.7992 213.3965 15.24980844191168Epoch: 2026-06-15T02:30Z
TLE epoch observation values (Epoch: 2026-06-15T02:30:41.772Z)
Latitude
-0.00003°
Longitude
-81.26347°
Altitude
500.495 km
Speed
7.611 km/s
True Right ascension
14h 39m 13s
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
01:16:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
495.638 km
Perigee altitude
479.959 km
Semi-major axis
6,865.935 km
Eccentricity
0.00114
Inclination
97.3195°
RAAN
219.8064°
Arg. of periapsis
146.7992°
True anomaly
213.32457°
Mean anomaly
213.3965°
Eccentric anomaly
213.36053°
Mean motion
3.81499 °/min
Orbital period
94.36 mins
BSTAR
0.00012731
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-15 15:41:42.383Z | 55.89° ENE | 2026-06-15 15:43:42.383Z | 98.195° ESE | 19.201° | 2026-06-15 15:45:42.383Z | 137.827° SSE |
| 4 mins | 2026-06-15 17:15:42.383Z | 321.064° NNW | 2026-06-15 17:16:42.383Z | 298.841° NW | 19.841° | 2026-06-15 17:19:42.383Z | 240.001° WSW |
| 5 mins | 2026-06-16 03:50:42.383Z | 183.196° SSW | 2026-06-16 03:52:42.383Z | 236.109° WSW | 40.82° | 2026-06-16 03:55:42.383Z | 338.398° N |
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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