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 29110U 06016D 23150.54899774 .00005725 00000-0 72853-3 0 9997
2 29110 98.4334 335.0173 0004207 58.3286 33.4258 14.81997604916799
| Epoch (UTC): | 30 May 2023 13:10:33 |
| Eccentricity: | 0.0004207 |
| inclination: | 98.4334° |
| perigee height: | 620 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 335.0173° |
| argument of perigee: | 58.3286° |
| revolutions per day: | 14.81997604 |
| mean anomaly at epoch: | 33.4258° |
| orbit number at epoch: | 91679 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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