CANX-5, 40056
Orbit data source: Space-Track
CANX-5, 40056 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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40056 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: 6 hours ago
TLE from 6 hours ago
0 CANX-5
1 40056U 14034D 25286.54286877 .00001571 00000-0 21204-3 0 9993
2 40056 98.3442 147.4074 0014271 83.8904 276.3933 14.80557360598836Epoch: 2025-10-13T13:01Z
TLE epoch observation values (Epoch: 2025-10-13T13:01:43.861Z)
Latitude
0.00001°
Longitude
-70.3695°
Altitude
629.475 km
Speed
7.544 km/s
True Right ascension
09h 49m 37s
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
13:37:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
634.62 km
Perigee altitude
614.632 km
Semi-major axis
7,002.763 km
Eccentricity
0.00143
Inclination
98.3442°
RAAN
147.4074°
Arg. of periapsis
83.8904°
True anomaly
276.23075°
Mean anomaly
276.3933°
Eccentric anomaly
276.31203°
Mean motion
3.70373 °/min
Orbital period
97.2 mins
BSTAR
0.00021204
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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-5 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 | 2025-10-14 04:11:55.021Z | 354.05° N | 2025-10-14 04:14:55.021Z | 285.143° WNW | 35.419° | 2025-10-14 04:18:55.021Z | 215.699° SW |
| 6 mins | 2025-10-14 15:06:55.021Z | 186.205° SSW | 2025-10-14 15:09:55.021Z | 283.447° WNW | 39.356° | 2025-10-14 15:12:55.021Z | 335.641° NNW |
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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