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 26065.65744279 +.00000000 +00000-0 -96457-4 0 00007
2 20625 70.9993 304.2832 0016205 303.6768 56.2809 14.15013556 04
| Epoch (UTC): | 06 March 2026 15:46:43 |
| Eccentricity: | 0.0016205 |
| inclination: | 70.9993° |
| perigee height: | 831 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 304.2832° |
| argument of perigee: | 303.6768° |
| revolutions per day: | 14.15013556 |
| mean anomaly at epoch: | 56.2809° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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