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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Edit Public Description
Identifier
Orbit
Country
Unknown / 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: 14 hours ago
TLE from 14 hours ago
0 ASTROCAST-0404
1 55112U 23001DH 26035.23546568 .00009275 00000-0 36611-3 0 9998
2 55112 97.5688 127.5581 0008564 104.4629 255.7560 15.25729298124240Epoch: 2026-02-04T05:39Z
TLE epoch observation values (Epoch: 2026-02-04T05:39:04.234Z)
Latitude
0.00001°
Longitude
-91.6145°
Altitude
493.142 km
Speed
7.617 km/s
True Right ascension
08h 30m 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
21:37:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
491.44 km
Perigee altitude
479.684 km
Semi-major axis
6,863.699 km
Eccentricity
0.00086
Inclination
97.5688°
RAAN
127.5581°
Arg. of periapsis
104.4629°
True anomaly
255.66091°
Mean anomaly
255.756°
Eccentric anomaly
255.70845°
Mean motion
3.81686 °/min
Orbital period
94.32 mins
BSTAR
0.00036611
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-02-05 05:24:28.419Z | 120.307° SE | 2026-02-05 05:26:28.419Z | 79.997° E | 22.617° | 2026-02-05 05:29:28.419Z | 17.167° NNE |
| 4 mins | 2026-02-05 18:26:28.419Z | 51.521° ENE | 2026-02-05 18:28:28.419Z | 113.723° SE | 27.682° | 2026-02-05 18:30:28.419Z | 156.462° SSE |
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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