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 68964U 26145.50003470 +.00000000 +00000-0 -20839-1 0 00007
2 68964 53.1594 268.3042 0001092 55.6668 23.0382 15.68160964 09
| Epoch (UTC): | 25 May 2026 12:00:02 |
| Eccentricity: | 0.0001092 |
| inclination: | 53.1594° |
| perigee height: | 363 km |
| apogee height: | 365 km |
| right ascension of ascending node: | 268.3042° |
| argument of perigee: | 55.6668° |
| revolutions per day: | 15.68160964 |
| mean anomaly at epoch: | 23.0382° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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