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 26042.25847480 +.00000000 +00000-0 +17976-3 0 00003
2 20625 71.0008 353.4213 0014854 336.5050 23.5392 14.15007650 01
| Epoch (UTC): | 11 February 2026 06:12:12 |
| Eccentricity: | 0.0014854 |
| inclination: | 71.0008° |
| perigee height: | 832 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 353.4213° |
| argument of perigee: | 336.5050° |
| revolutions per day: | 14.15007650 |
| mean anomaly at epoch: | 23.5392° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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