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: 5 hours ago
TLE from 5 hours ago
0 CONTINUUM-1
1 55045U 23001AN 26166.14801840 .00010470 00000-0 36029-3 0 9997
2 55045 97.3343 229.2674 0010674 73.9727 286.2689 15.30190145191949Epoch: 2026-06-15T03:33Z
TLE epoch observation values (Epoch: 2026-06-15T03:33:08.789Z)
Latitude
-0.00001°
Longitude
-87.45779°
Altitude
476.308 km
Speed
7.629 km/s
True Right ascension
15h 17m 04s
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
19:28:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
479.506 km
Perigee altitude
464.882 km
Semi-major axis
6,850.331 km
Eccentricity
0.00107
Inclination
97.3343°
RAAN
229.2674°
Arg. of periapsis
73.9727°
True anomaly
286.15144°
Mean anomaly
286.2689°
Eccentric anomaly
286.21017°
Mean motion
3.82803 °/min
Orbital period
94.04 mins
BSTAR
0.00036029
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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 | 2026-06-15 16:40:42.811Z | 34.894° NE | 2026-06-15 16:42:42.811Z | 78.937° E | 30.575° | 2026-06-15 16:45:42.811Z | 162.993° S |
| 4 mins | 2026-06-16 04:48:42.811Z | 221.356° SW | 2026-06-16 04:49:42.811Z | 250.616° W | 27.303° | 2026-06-16 04:52:42.811Z | 323.556° NNW |
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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