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 07715U 26161.64483799 +.00000000 +00000-0 +67460-5 0 00007
2 07715 81.2207 285.4757 0049956 263.5349 96.0131 14.07206577 04
| Epoch (UTC): | 10 June 2026 15:28:34 |
| Eccentricity: | 0.0049956 |
| inclination: | 81.2207° |
| perigee height: | 833 km |
| apogee height: | 905 km |
| right ascension of ascending node: | 285.4757° |
| argument of perigee: | 263.5349° |
| revolutions per day: | 14.07206577 |
| mean anomaly at epoch: | 96.0131° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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