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 26021.47499422 +.00000000 +00000-0 -34148-4 0 00005
2 20625 70.9995 37.0715 0013834 5.6699 354.4578 14.15008022 02
| Epoch (UTC): | 21 January 2026 11:23:59 |
| Eccentricity: | 0.0013834 |
| inclination: | 70.9995° |
| perigee height: | 832 km |
| apogee height: | 852 km |
| right ascension of ascending node: | 37.0715° |
| argument of perigee: | 5.6699° |
| revolutions per day: | 14.15008022 |
| mean anomaly at epoch: | 354.4578° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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