JAY-D1, 62669
Orbit data source: Space-Track
JAY-D1, 62669 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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62669 intel report (Beta)
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Edit Public Description
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, 0.5 m
Radar Cross Section
0.165 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 JAY-D1
1 62669U 25009BN 25290.93630276 .00007147 00000-0 33498-3 0 9998
2 62669 97.4265 9.0352 0006871 107.2024 252.9964 15.19972709 99545Epoch: 2025-10-17T22:28Z
TLE epoch observation values (Epoch: 2025-10-17T22:28:16.558Z)
Latitude
0.00001°
Longitude
5.29168°
Altitude
510.399 km
Speed
7.608 km/s
True Right ascension
00h 36m 08s
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
00:16:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.618 km
Perigee altitude
498.162 km
Semi-major axis
6,881.027 km
Eccentricity
0.00069
Inclination
97.4265°
RAAN
9.0352°
Arg. of periapsis
107.2024°
True anomaly
252.92112°
Mean anomaly
252.9964°
Eccentric anomaly
252.95876°
Mean motion
3.80245 °/min
Orbital period
94.68 mins
BSTAR
0.00033498
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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-D1 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 | 2025-10-18 18:00:14.380Z | 23.832° NE | 2025-10-18 18:02:14.380Z | 63.112° ENE | 39.23° | 2025-10-18 18:06:14.380Z | 181.605° SSW |
| 4 mins | 2025-10-19 04:39:14.380Z | 103.634° ESE | 2025-10-19 04:40:14.380Z | 81.148° E | 21.455° | 2025-10-19 04:43:14.380Z | 19.958° 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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