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 62789U 26145.57516183 +.00000000 +00000-0 +13256-3 0 00009
2 62789 88.9732 86.1101 0012137 229.1996 130.8104 13.51006157 06
| Epoch (UTC): | 25 May 2026 13:48:13 |
| Eccentricity: | 0.0012137 |
| inclination: | 88.9732° |
| perigee height: | 1060 km |
| apogee height: | 1078 km |
| right ascension of ascending node: | 86.1101° |
| argument of perigee: | 229.1996° |
| revolutions per day: | 13.51006157 |
| mean anomaly at epoch: | 130.8104° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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