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 22175.43402622 .00000209 00000-0 61748-4 0 9990
2 00029 48.3805 70.0575 0023667 146.7115 213.5291 14.74661052327296
| Epoch (UTC): | 24 June 2022 10:24:59 |
| Eccentricity: | 0.0023667 |
| inclination: | 48.3805° |
| perigee height: | 629 km |
| apogee height: | 663 km |
| right ascension of ascending node: | 70.0575° |
| argument of perigee: | 146.7115° |
| revolutions per day: | 14.74661052 |
| mean anomaly at epoch: | 213.5291° |
| orbit number at epoch: | 32729 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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