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 07318U 26106.02038875 +.00000000 +00000-0 +00000-0 0 00000
2 07318 2.0962 249.9905 0029365 346.8377 359.8986 1.01977889 09
| Epoch (UTC): | 16 April 2026 00:29:21 |
| Eccentricity: | 0.0029365 |
| inclination: | 2.0962° |
| perigee height: | 35193 km |
| apogee height: | 35437 km |
| right ascension of ascending node: | 249.9905° |
| argument of perigee: | 346.8377° |
| revolutions per day: | 1.01977889 |
| mean anomaly at epoch: | 359.8986° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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