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 02610U 26088.12276653 +.00000000 +00000-0 +30345-3 0 00006
2 02610 99.0980 291.8065 2272721 139.7745 239.5814 10.39828861 04
| Epoch (UTC): | 29 March 2026 02:56:47 |
| Eccentricity: | 0.2272721 |
| inclination: | 99.0980° |
| perigee height: | 473 km |
| apogee height: | 4504 km |
| right ascension of ascending node: | 291.8065° |
| argument of perigee: | 139.7745° |
| revolutions per day: | 10.39828861 |
| mean anomaly at epoch: | 239.5814° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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