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 26070.81794512 +.00000000 +00000-0 -72637-4 0 00000
2 20625 70.9983 293.4449 0016215 296.7590 63.1873 14.15011690 07
| Epoch (UTC): | 11 March 2026 19:37:50 |
| Eccentricity: | 0.0016215 |
| inclination: | 70.9983° |
| perigee height: | 831 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 293.4449° |
| argument of perigee: | 296.7590° |
| revolutions per day: | 14.15011690 |
| mean anomaly at epoch: | 63.1873° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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