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 26073.57492898 +.00000000 +00000-0 -92581-5 0 00009
2 20625 70.9977 287.6543 0016187 293.1130 66.8286 14.15011248 06
| Epoch (UTC): | 14 March 2026 13:47:53 |
| Eccentricity: | 0.0016187 |
| inclination: | 70.9977° |
| perigee height: | 831 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 287.6543° |
| argument of perigee: | 293.1130° |
| revolutions per day: | 14.15011248 |
| mean anomaly at epoch: | 66.8286° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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