EOSSAT-1, 55053
Orbit data source: Space-Track
EOSSAT-1, 55053 is a payload satellite owned by EOS DA (ZA) 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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55053 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / SAFRRelated business
Manufacturer
Dragonfly
Mission
Operational Commercial Imaging
Bus & Motor
EOS-SAT, AOCS
Mass
178 kg wet, 178 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl + 2 Pan, 0.3 m
Radar Cross Section
0.295 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 EOSSAT-1
1 55053U 23001AW 26024.12411103 .00012785 00000-0 42150-3 0 9999
2 55053 97.3451 86.0154 0008006 272.1749 87.8575 15.31553034169858Epoch: 2026-01-24T02:58Z
TLE epoch observation values (Epoch: 2026-01-24T02:58:43.192Z)
Latitude
-0.00013°
Longitude
-82.11763°
Altitude
474.085 km
Speed
7.629 km/s
True Right ascension
05h 44m 03s
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
21:03:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
473.607 km
Perigee altitude
462.645 km
Semi-major axis
6,846.263 km
Eccentricity
0.0008
Inclination
97.3451°
RAAN
86.0154°
Arg. of periapsis
272.1749°
True anomaly
87.94918°
Mean anomaly
87.8575°
Eccentric anomaly
87.90334°
Mean motion
3.83145 °/min
Orbital period
93.96 mins
BSTAR
0.0004215
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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.EOSSAT-1 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 | 2026-01-25 04:11:04.436Z | 175.297° S | 2026-01-25 04:14:04.436Z | 216.016° SW | 41.187° | 2026-01-25 04:17:04.436Z | 340.474° N |
| 5 mins | 2026-01-25 17:11:04.436Z | 350.972° N | 2026-01-25 17:13:04.436Z | 279.507° WNW | 37.233° | 2026-01-25 17:16:04.436Z | 210.903° SW |
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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