View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 63965U 26145.35642845 +.00000000 +00000-0 +67650-3 0 00004
2 63965 43.0010 103.0550 0001321 260.2773 99.7929 15.27597651 00
| Epoch (UTC): | 25 May 2026 08:33:15 |
| Eccentricity: | 0.0001321 |
| inclination: | 43.0010° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 103.0550° |
| argument of perigee: | 260.2773° |
| revolutions per day: | 15.27597651 |
| mean anomaly at epoch: | 99.7929° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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