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 63764U 26145.56765161 +.00000000 +00000-0 +63772-3 0 00002
2 63764 43.0028 331.1909 0000795 261.1496 98.9266 15.27595060 01
| Epoch (UTC): | 25 May 2026 13:37:25 |
| Eccentricity: | 0.0000795 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 331.1909° |
| argument of perigee: | 261.1496° |
| revolutions per day: | 15.27595060 |
| mean anomaly at epoch: | 98.9266° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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