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 22279.77769455 .00000853 00000-0 15627-3 0 9991
2 00029 48.3796 297.3610 0024456 233.5634 126.3023 14.74757407342692
| Epoch (UTC): | 06 October 2022 18:39:52 |
| Eccentricity: | 0.0024456 |
| inclination: | 48.3796° |
| perigee height: | 629 km |
| apogee height: | 663 km |
| right ascension of ascending node: | 297.3610° |
| argument of perigee: | 233.5634° |
| revolutions per day: | 14.74757407 |
| mean anomaly at epoch: | 126.3023° |
| orbit number at epoch: | 34269 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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