ASTROCAST-0404, 55112
Orbit data source: Space-Track
ASTROCAST-0404, 55112 is a payload satellite owned by Astrocast (CH) 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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55112 intel report (Beta)
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Identifier
Orbit
Country
CH / SWTZRelated business
Manufacturer
Astrocast
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
4.5 kg wet, 4.5 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 ASTROCAST-0404
1 55112U 23001DH 26278.25575533 .00026552 00000-0 88927-3 0 9997
2 55112 97.5647 14.2508 0005588 321.7649 38.3195 15.30905407161351Epoch: 2026-10-05T06:08Z
TLE epoch observation values (Epoch: 2026-10-05T06:08:17.260Z)
Latitude
0.00001°
Longitude
-91.75838°
Altitude
473.207 km
Speed
7.631 km/s
True Right ascension
00h 57m 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
12:02:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
473.895 km
Perigee altitude
466.241 km
Semi-major axis
6,848.205 km
Eccentricity
0.00056
Inclination
97.5647°
RAAN
14.2508°
Arg. of periapsis
321.7649°
True anomaly
38.35923°
Mean anomaly
38.3195°
Eccentric anomaly
38.33936°
Mean motion
3.82982 °/min
Orbital period
94 mins
BSTAR
0.00088927
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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.ASTROCAST-0404 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 | 2026-10-05 19:14:58.301Z | 19.569° NNE | 2026-10-05 19:17:58.301Z | 113.395° SE | 65.709° | 2026-10-05 19:20:58.301Z | 183.373° SSW |
| 4 mins | 2026-10-06 05:49:58.301Z | 99.852° ESE | 2026-10-06 05:50:58.301Z | 76.561° E | 21.677° | 2026-10-06 05:53:58.301Z | 18.396° NNE |
| 4 mins | 2026-10-06 07:22:58.301Z | 234.75° WSW | 2026-10-06 07:23:58.301Z | 256.2° W | 19.444° | 2026-10-06 07:26:58.301Z | 313.672° NW |
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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