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 62822U 26145.46422602 +.00000000 +00000-0 +60868-3 0 00008
2 62822 53.1585 312.9313 0001598 107.6908 252.4267 15.30216317 02
| Epoch (UTC): | 25 May 2026 11:08:29 |
| Eccentricity: | 0.0001598 |
| inclination: | 53.1585° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 312.9313° |
| argument of perigee: | 107.6908° |
| revolutions per day: | 15.30216317 |
| mean anomaly at epoch: | 252.4267° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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