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 63881U 26145.44132312 +.00000000 +00000-0 +17360-3 0 00007
2 63881 70.0023 40.7894 0002854 270.1209 89.9623 14.98332353 00
| Epoch (UTC): | 25 May 2026 10:35:30 |
| Eccentricity: | 0.0002854 |
| inclination: | 70.0023° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 40.7894° |
| argument of perigee: | 270.1209° |
| revolutions per day: | 14.98332353 |
| mean anomaly at epoch: | 89.9623° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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