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: 11 hours ago
TLE from 11 hours ago
0 CONTINUUM-1
1 55045U 23001AN 26278.29594354 .00013456 00000-0 41571-3 0 9991
2 55045 97.3245 340.2644 0009392 62.4926 297.7271 15.33608857209110Epoch: 2026-10-05T07:06Z
TLE epoch observation values (Epoch: 2026-10-05T07:06:09.521Z)
Latitude
0.00003°
Longitude
-140.25215°
Altitude
465.181 km
Speed
7.635 km/s
True Right ascension
22h 41m 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
11:58:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
468.424 km
Perigee altitude
455.576 km
Semi-major axis
6,840.137 km
Eccentricity
0.00094
Inclination
97.3245°
RAAN
340.2644°
Arg. of periapsis
62.4926°
True anomaly
297.63178°
Mean anomaly
297.7271°
Eccentric anomaly
297.67945°
Mean motion
3.8366 °/min
Orbital period
93.83 mins
BSTAR
0.00041571
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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.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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-10-06 03:36:10.327Z | 120.909° SE | 2026-10-06 03:38:10.327Z | 83.067° E | 22.242° | 2026-10-06 03:41:10.327Z | 19.451° NNE |
| 4 mins | 2026-10-06 16:34:10.327Z | 50.717° ENE | 2026-10-06 16:36:10.327Z | 105.561° ESE | 28.258° | 2026-10-06 16:38:10.327Z | 150.586° SSE |
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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