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 26071.73693959 +.00000000 +00000-0 -52625-4 0 00000
2 20625 70.9981 291.5148 0016198 295.5364 64.4084 14.15011499 01
| Epoch (UTC): | 12 March 2026 17:41:11 |
| Eccentricity: | 0.0016198 |
| inclination: | 70.9981° |
| perigee height: | 831 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 291.5148° |
| argument of perigee: | 295.5364° |
| revolutions per day: | 14.15011499 |
| mean anomaly at epoch: | 64.4084° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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