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 23156.55083343 .00005980 00000-0 75929-3 0 9991
2 29110 98.4326 341.3363 0003915 42.3949 11.8621 14.82071783917680
| Epoch (UTC): | 05 June 2023 13:13:12 |
| Eccentricity: | 0.0003915 |
| inclination: | 98.4326° |
| perigee height: | 620 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 341.3363° |
| argument of perigee: | 42.3949° |
| revolutions per day: | 14.82071783 |
| mean anomaly at epoch: | 11.8621° |
| orbit number at epoch: | 91768 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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