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 22333.57205948 .00000258 00000-0 68648-4 0 9993
2 00029 48.3808 43.3072 0023336 103.2800 257.0716 14.74840471350639
| Epoch (UTC): | 29 November 2022 13:43:45 |
| Eccentricity: | 0.0023336 |
| inclination: | 48.3808° |
| perigee height: | 629 km |
| apogee height: | 662 km |
| right ascension of ascending node: | 43.3072° |
| argument of perigee: | 103.2800° |
| revolutions per day: | 14.74840471 |
| mean anomaly at epoch: | 257.0716° |
| orbit number at epoch: | 35063 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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