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 26105.73963755 +.00000000 +00000-0 -12554-3 0 00008
2 20625 70.9994 220.0977 0016485 251.3380 108.5953 14.15016658 06
| Epoch (UTC): | 15 April 2026 17:45:04 |
| Eccentricity: | 0.0016485 |
| inclination: | 70.9994° |
| perigee height: | 830 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 220.0977° |
| argument of perigee: | 251.3380° |
| revolutions per day: | 14.15016658 |
| mean anomaly at epoch: | 108.5953° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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