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 26019.28354270 +.00000000 +00000-0 -23986-4 0 00000
2 20625 70.9995 41.6741 0013711 9.1001 351.0367 14.15007879 00
| Epoch (UTC): | 19 January 2026 06:48:18 |
| Eccentricity: | 0.0013711 |
| inclination: | 70.9995° |
| perigee height: | 832 km |
| apogee height: | 852 km |
| right ascension of ascending node: | 41.6741° |
| argument of perigee: | 9.1001° |
| revolutions per day: | 14.15007879 |
| mean anomaly at epoch: | 351.0367° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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