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 62182U 26145.48865819 +.00000000 +00000-0 +20614-3 0 00005
2 62182 70.0019 330.6260 0002022 272.7942 87.2985 14.98335110 01
| Epoch (UTC): | 25 May 2026 11:43:40 |
| Eccentricity: | 0.0002022 |
| inclination: | 70.0019° |
| perigee height: | 571 km |
| apogee height: | 573 km |
| right ascension of ascending node: | 330.6260° |
| argument of perigee: | 272.7942° |
| revolutions per day: | 14.98335110 |
| mean anomaly at epoch: | 87.2985° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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