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 62804U 26145.58736845 +.00000000 +00000-0 +00000-0 0 00007
2 62804 0.8327 294.1833 0000060 147.7106 31.1286 1.00275114 06
| Epoch (UTC): | 25 May 2026 14:05:48 |
| Eccentricity: | 0.0000060 |
| inclination: | 0.8327° |
| perigee height: | 35785 km |
| apogee height: | 35786 km |
| right ascension of ascending node: | 294.1833° |
| argument of perigee: | 147.7106° |
| revolutions per day: | 1.00275114 |
| mean anomaly at epoch: | 31.1286° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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