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 62628U 26145.40468199 +.00000000 +00000-0 +57547-3 0 00007
2 62628 97.4310 186.0167 0593188 177.7741 182.6326 14.49828506 02
| Epoch (UTC): | 25 May 2026 09:42:44 |
| Eccentricity: | 0.0593188 |
| inclination: | 97.4310° |
| perigee height: | 305 km |
| apogee height: | 1148 km |
| right ascension of ascending node: | 186.0167° |
| argument of perigee: | 177.7741° |
| revolutions per day: | 14.49828506 |
| mean anomaly at epoch: | 182.6326° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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