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 00716U 26161.03774139 +.00000000 +00000-0 +71901-4 0 00009
2 00716 58.4949 62.7364 0015501 244.8284 115.1148 14.73171715 05
| Epoch (UTC): | 10 June 2026 00:54:20 |
| Eccentricity: | 0.0015501 |
| inclination: | 58.4949° |
| perigee height: | 640 km |
| apogee height: | 662 km |
| right ascension of ascending node: | 62.7364° |
| argument of perigee: | 244.8284° |
| revolutions per day: | 14.73171715 |
| mean anomaly at epoch: | 115.1148° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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