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: 16 hours ago
TLE from 16 hours ago
0 CANX-5
1 40056U 14034D 25256.06167416 .00000750 00000-0 10552-3 0 9996
2 40056 98.3503 115.7075 0012912 175.8283 184.3038 14.80436926594323Epoch: 2025-09-13T01:28Z
TLE epoch observation values (Epoch: 2025-09-13T01:28:48.647Z)
Latitude
0.00001°
Longitude
101.20437°
Altitude
639.976 km
Speed
7.533 km/s
True Right ascension
07h 42m 49s
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
09:36:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
634.049 km
Perigee altitude
615.964 km
Semi-major axis
7,003.143 km
Eccentricity
0.00129
Inclination
98.3503°
RAAN
115.7075°
Arg. of periapsis
175.8283°
True anomaly
184.29271°
Mean anomaly
184.3038°
Eccentric anomaly
184.29826°
Mean motion
3.70343 °/min
Orbital period
97.21 mins
BSTAR
0.00010552
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-14 04:00:41.895Z | 356.238° N | 2025-09-14 04:03:41.895Z | 275.058° WNW | 37.816° | 2025-09-14 04:06:41.895Z | 215.331° SW |
| 6 mins | 2025-09-14 14:55:41.895Z | 181.495° SSW | 2025-09-14 14:57:41.895Z | 222.768° SW | 41.412° | 2025-09-14 15:01:41.895Z | 339.335° N |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
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