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 62290U 26145.58809560 +.00000000 +00000-0 +72285-4 0 00009
2 62290 59.9148 355.0640 0014555 217.0418 142.9586 13.75217502 01
| Epoch (UTC): | 25 May 2026 14:06:51 |
| Eccentricity: | 0.0014555 |
| inclination: | 59.9148° |
| perigee height: | 970 km |
| apogee height: | 992 km |
| right ascension of ascending node: | 355.0640° |
| argument of perigee: | 217.0418° |
| revolutions per day: | 13.75217502 |
| mean anomaly at epoch: | 142.9586° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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