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 00029U 60002B 23338.70697333 .00001523 00000-0 24910-3 0 9996
2 00029 48.3775 93.9202 0024103 249.9608 109.8709 14.75786616405284
| Epoch (UTC): | 04 December 2023 16:58:02 |
| Eccentricity: | 0.0024103 |
| inclination: | 48.3775° |
| perigee height: | 626 km |
| apogee height: | 659 km |
| right ascension of ascending node: | 93.9202° |
| argument of perigee: | 249.9608° |
| revolutions per day: | 14.75786616 |
| mean anomaly at epoch: | 109.8709° |
| orbit number at epoch: | 40528 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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