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 00979U 26135.19373859 +.00000000 +00000-0 +79670-4 0 00003
2 00979 96.4204 7.7937 1138604 333.9402 20.8348 12.15525289 07
| Epoch (UTC): | 15 May 2026 04:38:59 |
| Eccentricity: | 0.1138604 |
| inclination: | 96.4204° |
| perigee height: | 702 km |
| apogee height: | 2522 km |
| right ascension of ascending node: | 7.7937° |
| argument of perigee: | 333.9402° |
| revolutions per day: | 12.15525289 |
| mean anomaly at epoch: | 20.8348° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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