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 25695U 26088.12412795 +.00000000 +00000-0 +10111-3 0 00002
2 25695 64.5568 6.1416 0561054 326.6165 30.0643 13.73039838 02
| Epoch (UTC): | 29 March 2026 02:58:44 |
| Eccentricity: | 0.0561054 |
| inclination: | 64.5568° |
| perigee height: | 575 km |
| apogee height: | 1402 km |
| right ascension of ascending node: | 6.1416° |
| argument of perigee: | 326.6165° |
| revolutions per day: | 13.73039838 |
| mean anomaly at epoch: | 30.0643° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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