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 23151.67027659 .00000629 00000-0 12186-3 0 9991
2 00029 48.3790 258.2404 0023605 169.1288 191.0139 14.75328372377665
| Epoch (UTC): | 31 May 2023 16:05:11 |
| Eccentricity: | 0.0023605 |
| inclination: | 48.3790° |
| perigee height: | 627 km |
| apogee height: | 660 km |
| right ascension of ascending node: | 258.2404° |
| argument of perigee: | 169.1288° |
| revolutions per day: | 14.75328372 |
| mean anomaly at epoch: | 191.0139° |
| orbit number at epoch: | 37766 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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