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 20666U 90055D 25188.63834724 .00001501 00000-0 12812-3 0 9994
2 20666 62.7839 6.1576 0023357 196.7370 163.2961 15.02099080901366
| Epoch (UTC): | 07 July 2025 15:19:13 |
| Eccentricity: | 0.0023357 |
| inclination: | 62.7839° |
| perigee height: | 544 km |
| apogee height: | 576 km |
| right ascension of ascending node: | 6.1576° |
| argument of perigee: | 196.7370° |
| revolutions per day: | 15.02099080 |
| mean anomaly at epoch: | 163.2961° |
| orbit number at epoch: | 90136 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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