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 21528U 91045B 23340.45177575 .00000629 00000-0 24969-3 0 9990
2 21528 89.5385 310.1409 0068019 12.3507 102.1160 14.26502885685818
| Epoch (UTC): | 06 December 2023 10:50:33 |
| Eccentricity: | 0.0068019 |
| inclination: | 89.5385° |
| perigee height: | 754 km |
| apogee height: | 852 km |
| right ascension of ascending node: | 310.1409° |
| argument of perigee: | 12.3507° |
| revolutions per day: | 14.26502885 |
| mean anomaly at epoch: | 102.1160° |
| orbit number at epoch: | 68581 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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