JAY-D2, 62665
Orbit data source: Space-Track
JAY-D2, 62665 is a Canadian payload satellite in SSO that was launched on Tue, 14 Jan 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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62665 intel report (Beta)
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Identifier
Orbit
Country
CARelated business
Manufacturer
UTIAS-SFL
Mission
Operational Commercial Imaging
Bus & Motor
DEFIANT, Unknown motor
Mass
~35 kg wet, ~35 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.3 m
Radar Cross Section
0.165 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 JAY-D2
1 62665U 25009BJ 26287.58769962 .00003370 00000-0 14623-3 0 9990
2 62665 97.3798 4.0447 0002699 270.4084 89.6843 15.23014813 96900Epoch: 2026-10-14T14:06Z
TLE epoch observation values (Epoch: 2026-10-14T14:06:17.247Z)
Latitude
-0.00006°
Longitude
129.33757°
Altitude
499.838 km
Speed
7.615 km/s
True Right ascension
00h 16m 10s
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
03:12:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
495.568 km
Perigee altitude
491.859 km
Semi-major axis
6,871.851 km
Eccentricity
0.00027
Inclination
97.3798°
RAAN
4.0447°
Arg. of periapsis
270.4084°
True anomaly
89.71523°
Mean anomaly
89.6843°
Eccentric anomaly
89.69976°
Mean motion
3.81007 °/min
Orbital period
94.49 mins
BSTAR
0.00014623
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Other satellites on launch #9 in the year 2025 (2025-01-14 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.JAY-D2 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 | 2026-10-15 17:28:28.143Z | 35.66° NE | 2026-10-15 17:31:28.143Z | 90.092° ESE | 27.77° | 2026-10-15 17:34:28.143Z | 153.773° SSE |
| 5 mins | 2026-10-16 05:39:28.143Z | 195.63° SSW | 2026-10-16 05:41:28.143Z | 241.831° WSW | 41.499° | 2026-10-16 05:44:28.143Z | 328.552° 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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