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 30798U 26145.58832178 +.00000000 +00000-0 +00000-0 0 00000
2 30798 6.0976 99.4502 8444797 211.4155 128.9201 0.88041996 06
| Epoch (UTC): | 25 May 2026 14:07:11 |
| Eccentricity: | 0.8444797 |
| inclination: | 6.0976° |
| perigee height: | 773 km |
| apogee height: | 78439 km |
| right ascension of ascending node: | 99.4502° |
| argument of perigee: | 211.4155° |
| revolutions per day: | 0.88041996 |
| mean anomaly at epoch: | 128.9201° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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