CANX-4, 40055
Orbit data source: Space-Track
CANX-4, 40055 is a payload satellite owned by UTIAS-SFL (CA) in SSO that was launched on Mon, 30 Jun 2014 UTC via a PSLV launch vehicle from the Sirharikota (SRI). 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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40055 intel report (Beta)
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Identifier
Orbit
Country
CARelated business
Manufacturer
UTIAS-SFL
Mission
Operational Amateur Technology
Bus & Motor
GNB, Unknown motor
Mass
7 kg wet, 7 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 4 Ant, 0.2 m
Radar Cross Section
0.060 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 CANX-4
1 40055U 14034C 26276.90242902 .00000454 00000-0 65341-4 0 9993
2 40055 98.2930 156.1131 0013352 26.7391 333.4507 14.81416554660621Epoch: 2026-10-03T21:39Z
TLE epoch observation values (Epoch: 2026-10-03T21:39:29.867Z)
Latitude
0.00006°
Longitude
178.63528°
Altitude
619.504 km
Speed
7.554 km/s
True Right ascension
10h 24m 27s
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
22:43:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
631.26 km
Perigee altitude
612.567 km
Semi-major axis
7,000.05 km
Eccentricity
0.00134
Inclination
98.293°
RAAN
156.1131°
Arg. of periapsis
26.7391°
True anomaly
333.38221°
Mean anomaly
333.4507°
Eccentric anomaly
333.41647°
Mean motion
3.70588 °/min
Orbital period
97.14 mins
BSTAR
0.000065341
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Other satellites on launch #34 in the year 2014 (2014-06-30 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.CANX-4 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 | 2026-10-04 15:38:06.150Z | 134.341° SE | 2026-10-04 15:40:06.150Z | 92.709° ESE | 42.791° | 2026-10-04 15:44:06.150Z | 2.749° 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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