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 23154.52719234 .00005991 00000-0 76109-3 0 9994
2 29110 98.4324 339.2057 0004004 47.8743 15.9118 14.82047224917382
| Epoch (UTC): | 03 June 2023 12:39:09 |
| Eccentricity: | 0.0004004 |
| inclination: | 98.4324° |
| perigee height: | 620 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 339.2057° |
| argument of perigee: | 47.8743° |
| revolutions per day: | 14.82047224 |
| mean anomaly at epoch: | 15.9118° |
| orbit number at epoch: | 91738 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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