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 22275.50924501 .00000548 00000-0 11142-3 0 9992
2 00029 48.3801 317.5181 0024353 215.5145 144.4147 14.74748705342060
| Epoch (UTC): | 02 October 2022 12:13:18 |
| Eccentricity: | 0.0024353 |
| inclination: | 48.3801° |
| perigee height: | 629 km |
| apogee height: | 663 km |
| right ascension of ascending node: | 317.5181° |
| argument of perigee: | 215.5145° |
| revolutions per day: | 14.74748705 |
| mean anomaly at epoch: | 144.4147° |
| orbit number at epoch: | 34206 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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