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 data is extracted from the following two-line orbital elements,
1 20491U 90013D 25322.43237513 .00000194 00000-0 43403-3 0 9992
2 20491 99.0371 291.1470 0467132 292.1015 63.1135 13.03740781701566
| Epoch (UTC): | 18 November 2025 10:22:37 |
| Eccentricity: | 0.0467132 |
| inclination: | 99.0371° |
| perigee height: | 891 km |
| apogee height: | 1603 km |
| right ascension of ascending node: | 291.1470° |
| argument of perigee: | 292.1015° |
| revolutions per day: | 13.03740781 |
| mean anomaly at epoch: | 63.1135° |
| orbit number at epoch: | 70156 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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