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 62790U 26145.60807380 +.00000000 +00000-0 +15007-3 0 00003
2 62790 88.9713 86.0470 0013747 225.4830 134.5199 13.51008575 00
| Epoch (UTC): | 25 May 2026 14:35:37 |
| Eccentricity: | 0.0013747 |
| inclination: | 88.9713° |
| perigee height: | 1058 km |
| apogee height: | 1079 km |
| right ascension of ascending node: | 86.0470° |
| argument of perigee: | 225.4830° |
| revolutions per day: | 13.51008575 |
| mean anomaly at epoch: | 134.5199° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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