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 23342.49848574 .00000703 00000-0 13127-3 0 9999
2 00029 48.3795 75.9872 0024189 265.8555 93.9592 14.75793790405847
| Epoch (UTC): | 08 December 2023 11:57:49 |
| Eccentricity: | 0.0024189 |
| inclination: | 48.3795° |
| perigee height: | 625 km |
| apogee height: | 659 km |
| right ascension of ascending node: | 75.9872° |
| argument of perigee: | 265.8555° |
| revolutions per day: | 14.75793790 |
| mean anomaly at epoch: | 93.9592° |
| orbit number at epoch: | 40584 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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