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 23152.92052748 .00006452 00000-0 81944-3 0 9992
2 29110 98.4327 337.5142 0004069 51.9621 84.8831 14.82028761917149
| Epoch (UTC): | 01 June 2023 22:05:33 |
| Eccentricity: | 0.0004069 |
| inclination: | 98.4327° |
| perigee height: | 620 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 337.5142° |
| argument of perigee: | 51.9621° |
| revolutions per day: | 14.82028761 |
| mean anomaly at epoch: | 84.8831° |
| orbit number at epoch: | 91714 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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