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 22277.06757002 .00000739 00000-0 13952-3 0 9998
2 00029 48.3799 310.1591 0024396 222.1259 137.7778 14.74752093342292
| Epoch (UTC): | 04 October 2022 01:37:18 |
| Eccentricity: | 0.0024396 |
| inclination: | 48.3799° |
| perigee height: | 629 km |
| apogee height: | 663 km |
| right ascension of ascending node: | 310.1591° |
| argument of perigee: | 222.1259° |
| revolutions per day: | 14.74752093 |
| mean anomaly at epoch: | 137.7778° |
| orbit number at epoch: | 34229 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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