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 25724U 99023A 20366.20381350 0.00000030 00000-0 37321-3 0 07
2 25724 28.2666 73.0372 2135793 340.4162 19.5833 9.37474133 04
| Epoch (UTC): | 31 December 2020 04:53:29 |
| Eccentricity: | 0.2135793 |
| inclination: | 28.2666° |
| perigee height: | 1093 km |
| apogee height: | 5152 km |
| right ascension of ascending node: | 73.0372° |
| argument of perigee: | 340.4162° |
| revolutions per day: | 9.37474133 |
| mean anomaly at epoch: | 19.5833° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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