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 25189.20164992 .00011843 00000-0 77010-3 0 9999
2 29110 98.3511 75.9033 0007161 67.1842 92.9530 15.08153028 31580
| Epoch (UTC): | 08 July 2025 04:50:22 |
| Eccentricity: | 0.0007161 |
| inclination: | 98.3511° |
| perigee height: | 537 km |
| apogee height: | 547 km |
| right ascension of ascending node: | 75.9033° |
| argument of perigee: | 67.1842° |
| revolutions per day: | 15.08153028 |
| mean anomaly at epoch: | 92.9530° |
| orbit number at epoch: | 3158 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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