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 62180U 26145.50534722 +.00000000 +00000-0 +30314-3 0 00000
2 62180 70.0027 330.5937 0002846 267.4418 92.6415 14.98338564 05
| Epoch (UTC): | 25 May 2026 12:07:42 |
| Eccentricity: | 0.0002846 |
| inclination: | 70.0027° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 330.5937° |
| argument of perigee: | 267.4418° |
| revolutions per day: | 14.98338564 |
| mean anomaly at epoch: | 92.6415° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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