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 62117U 26145.47855355 +.00000000 +00000-0 +49222-3 0 00002
2 62117 43.0005 58.8771 0000443 336.5906 23.4925 15.27592748 05
| Epoch (UTC): | 25 May 2026 11:29:07 |
| Eccentricity: | 0.0000443 |
| inclination: | 43.0005° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 58.8771° |
| argument of perigee: | 336.5906° |
| revolutions per day: | 15.27592748 |
| mean anomaly at epoch: | 23.4925° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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