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 62799U 26145.59984397 +.00000000 +00000-0 +12758-3 0 00004
2 62799 88.9709 85.9342 0013760 227.3450 132.6543 13.51012568 03
| Epoch (UTC): | 25 May 2026 14:23:46 |
| Eccentricity: | 0.0013760 |
| inclination: | 88.9709° |
| perigee height: | 1058 km |
| apogee height: | 1079 km |
| right ascension of ascending node: | 85.9342° |
| argument of perigee: | 227.3450° |
| revolutions per day: | 13.51012568 |
| mean anomaly at epoch: | 132.6543° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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