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 63945U 26145.22499728 +.00000000 +00000-0 +29536-3 0 00009
2 63945 70.0012 81.6098 0003090 267.2299 92.8507 14.98336960 00
| Epoch (UTC): | 25 May 2026 05:23:59 |
| Eccentricity: | 0.0003090 |
| inclination: | 70.0012° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 81.6098° |
| argument of perigee: | 267.2299° |
| revolutions per day: | 14.98336960 |
| mean anomaly at epoch: | 92.8507° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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