CONTINUUM-1, 55045
Orbit data source: Space-Track
CONTINUUM-1, 55045 is a payload satellite owned by URUGUS S.A. (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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55045 intel report (Beta)
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Identifier
Orbit
Country
AU / AUSRelated business
Manufacturer
URUGUS S.A.
Mission
Operational Commercial Imaging
Bus & Motor
NEWSAT IVG, Unknown motor
Mass
41.5 kg wet, 38.5 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 1.0 m
Radar Cross Section
0.542 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 CONTINUUM-1
1 55045U 23001AN 26227.90911745 .00008121 00000-0 25992-3 0 9992
2 55045 97.3314 290.3313 0007309 224.6531 135.4123 15.32638248201397Epoch: 2026-08-15T21:49Z
TLE epoch observation values (Epoch: 2026-08-15T21:49:07.747Z)
Latitude
-0.00006°
Longitude
-1.26421°
Altitude
474.62 km
Speed
7.627 km/s
True Right ascension
19h 21m 19s
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
18:38:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
469.892 km
Perigee altitude
459.889 km
Semi-major axis
6,843.027 km
Eccentricity
0.00073
Inclination
97.3314°
RAAN
290.3313°
Arg. of periapsis
224.6531°
True anomaly
135.47106°
Mean anomaly
135.4123°
Eccentric anomaly
135.44168°
Mean motion
3.83416 °/min
Orbital period
93.89 mins
BSTAR
0.00025992
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Other satellites on launch #1 in the year 2023 (2023-01-03 UTC)
Did you know?
You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.CONTINUUM-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 | 2026-08-16 04:12:26.320Z | 163.03° S | 2026-08-16 04:15:26.320Z | 133.791° SE | 43.224° | 2026-08-16 04:18:26.320Z | 351.693° N |
| 5 mins | 2026-08-16 17:11:26.320Z | 7.279° NNE | 2026-08-16 17:13:26.320Z | 338.166° N | 43.025° | 2026-08-16 17:16:26.320Z | 198.171° SSW |
| 5 mins | 2026-08-17 03:44:26.320Z | 122.235° SE | 2026-08-17 03:46:26.320Z | 70.085° E | 26.531° | 2026-08-17 03:49:26.320Z | 10.282° NNE |
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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