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 02680U 26106.45132742 +.00000000 +00000-0 +33395-3 0 00008
2 02680 39.4393 13.1534 0698892 50.8093 315.2627 13.41917529 01
| Epoch (UTC): | 16 April 2026 10:49:54 |
| Eccentricity: | 0.0698892 |
| inclination: | 39.4393° |
| perigee height: | 579 km |
| apogee height: | 1625 km |
| right ascension of ascending node: | 13.1534° |
| argument of perigee: | 50.8093° |
| revolutions per day: | 13.41917529 |
| mean anomaly at epoch: | 315.2627° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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