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 26064.95052528 +.00000000 +00000-0 -93291-4 0 00001
2 20625 70.9995 305.7678 0016196 304.5886 55.3708 14.15013791 09
| Epoch (UTC): | 05 March 2026 22:48:45 |
| Eccentricity: | 0.0016196 |
| inclination: | 70.9995° |
| perigee height: | 831 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 305.7678° |
| argument of perigee: | 304.5886° |
| revolutions per day: | 14.15013791 |
| mean anomaly at epoch: | 55.3708° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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