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 20442U 90005G 25073.79218994 .00000463 00000-0 18296-3 0 9994
2 20442 98.9003 77.4973 0012683 111.1694 249.0846 14.33887775836613
| Epoch (UTC): | 14 March 2025 19:00:45 |
| Eccentricity: | 0.0012683 |
| inclination: | 98.9003° |
| perigee height: | 769 km |
| apogee height: | 788 km |
| right ascension of ascending node: | 77.4973° |
| argument of perigee: | 111.1694° |
| revolutions per day: | 14.33887775 |
| mean anomaly at epoch: | 249.0846° |
| orbit number at epoch: | 83661 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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