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, 0.1 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 ASTROCAST-0404
1 55112U 23001DH 26181.23222004 .00006819 00000-0 24767-3 0 9996
2 55112 97.5675 275.5464 0005008 312.8600 47.2218 15.28620696146528Epoch: 2026-06-30T05:34Z
TLE epoch observation values (Epoch: 2026-06-30T05:34:23.811Z)
Latitude
-0.00004°
Longitude
-86.35908°
Altitude
480.7 km
Speed
7.626 km/s
True Right ascension
18h 22m 11s
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
23:30:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
480.329 km
Perigee altitude
473.463 km
Semi-major axis
6,855.033 km
Eccentricity
0.0005
Inclination
97.5675°
RAAN
275.5464°
Arg. of periapsis
312.86°
True anomaly
47.26394°
Mean anomaly
47.2218°
Eccentric anomaly
47.24287°
Mean motion
3.8241 °/min
Orbital period
94.14 mins
BSTAR
0.00024767
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-07-01 18:17:24.411Z | 57.816° ENE | 2026-07-01 18:19:24.411Z | 94.3° ESE | 15.531° | 2026-07-01 18:21:24.411Z | 130.541° SE |
| 4 mins | 2026-07-01 19:51:24.411Z | 324.776° NNW | 2026-07-01 19:52:24.411Z | 298.87° NW | 24.253° | 2026-07-01 19:55:24.411Z | 233.018° WSW |
| 5 mins | 2026-07-02 06:25:24.411Z | 172.363° S | 2026-07-02 06:27:24.411Z | 328.328° NNW | 42.905° | 2026-07-02 06:30:24.411Z | 346.061° 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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