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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Edit Public Description
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, 0.1 m
Radar Cross Section
0.060 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 CANX-4
1 40055U 14034C 25309.58697878 .00001471 00000-0 19880-3 0 9995
2 40055 98.3400 171.3331 0013347 15.0865 345.0742 14.80625652611431Epoch: 2025-11-05T14:05Z
TLE epoch observation values (Epoch: 2025-11-05T14:05:14.966Z)
Latitude
0.00003°
Longitude
-85.03677°
Altitude
621.323 km
Speed
7.553 km/s
True Right ascension
11h 25m 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
05:11:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
633.757 km
Perigee altitude
615.064 km
Semi-major axis
7,002.547 km
Eccentricity
0.00133
Inclination
98.34°
RAAN
171.3331°
Arg. of periapsis
15.0865°
True anomaly
345.03474°
Mean anomaly
345.0742°
Eccentric anomaly
345.05448°
Mean motion
3.7039 °/min
Orbital period
97.19 mins
BSTAR
0.0001988
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-11-06 14:32:47.154Z | 144.781° SSE | 2025-11-06 14:35:47.154Z | 90.652° ESE | 37.149° | 2025-11-06 14:39:47.154Z | 359.493° N |
| 7 mins | 2025-11-07 03:57:47.154Z | 8.241° NNE | 2025-11-07 04:00:47.154Z | 321.461° NNW | 43.611° | 2025-11-07 04:04:47.154Z | 200.743° SSW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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