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 30797U 26145.26854484 +.00000000 +00000-0 +00000-0 0 00008
2 30797 7.4778 81.4336 8336031 227.5290 254.2022 0.87589238 04
| Epoch (UTC): | 25 May 2026 06:26:42 |
| Eccentricity: | 0.8336031 |
| inclination: | 7.4778° |
| perigee height: | 1300 km |
| apogee height: | 78229 km |
| right ascension of ascending node: | 81.4336° |
| argument of perigee: | 227.5290° |
| revolutions per day: | 0.87589238 |
| mean anomaly at epoch: | 254.2022° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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