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 23344.25882605 .00000615 00000-0 11864-3 0 9996
2 00029 48.3797 67.6607 0024201 273.1859 86.6284 14.75797086406106
| Epoch (UTC): | 10 December 2023 06:12:42 |
| Eccentricity: | 0.0024201 |
| inclination: | 48.3797° |
| perigee height: | 625 km |
| apogee height: | 659 km |
| right ascension of ascending node: | 67.6607° |
| argument of perigee: | 273.1859° |
| revolutions per day: | 14.75797086 |
| mean anomaly at epoch: | 86.6284° |
| orbit number at epoch: | 40610 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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