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 62245U 26145.49979925 +.00000000 +00000-0 +13428-3 0 00005
2 62245 89.0101 24.6170 0015737 80.3866 279.9062 13.51007683 03
| Epoch (UTC): | 25 May 2026 11:59:42 |
| Eccentricity: | 0.0015737 |
| inclination: | 89.0101° |
| perigee height: | 1057 km |
| apogee height: | 1080 km |
| right ascension of ascending node: | 24.6170° |
| argument of perigee: | 80.3866° |
| revolutions per day: | 13.51007683 |
| mean anomaly at epoch: | 279.9062° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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