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 25635U 26100.22266304 +.00000000 +00000-0 +19812-3 0 00002
2 25635 96.4829 23.1723 0133202 45.1964 315.9975 14.51735922 07
| Epoch (UTC): | 10 April 2026 05:20:38 |
| Eccentricity: | 0.0133202 |
| inclination: | 96.4829° |
| perigee height: | 625 km |
| apogee height: | 815 km |
| right ascension of ascending node: | 23.1723° |
| argument of perigee: | 45.1964° |
| revolutions per day: | 14.51735922 |
| mean anomaly at epoch: | 315.9975° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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