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 21903U 92012B 24287.31161889 .00000236 00000-0 23094-3 0 9991
2 21903 82.9412 1.9791 0042505 194.4887 231.1699 13.74678461634806
| Epoch (UTC): | 13 October 2024 07:28:43 |
| Eccentricity: | 0.0042505 |
| inclination: | 82.9412° |
| perigee height: | 951 km |
| apogee height: | 1014 km |
| right ascension of ascending node: | 1.9791° |
| argument of perigee: | 194.4887° |
| revolutions per day: | 13.74678461 |
| mean anomaly at epoch: | 231.1699° |
| orbit number at epoch: | 63480 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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