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 20625U 26072.93870190 +.00000000 +00000-0 -26331-4 0 00002
2 20625 70.9978 288.9905 0016190 293.9574 65.9853 14.15011256 06
| Epoch (UTC): | 13 March 2026 22:31:43 |
| Eccentricity: | 0.0016190 |
| inclination: | 70.9978° |
| perigee height: | 831 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 288.9905° |
| argument of perigee: | 293.9574° |
| revolutions per day: | 14.15011256 |
| mean anomaly at epoch: | 65.9853° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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