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 26729U 89006G 24280.30589923 .00000438 00000-0 27255-2 0 9992
2 26729 7.9692 220.8249 7173088 155.1177 271.4014 2.30714324198035
| Epoch (UTC): | 06 October 2024 07:20:29 |
| Eccentricity: | 0.7173088 |
| inclination: | 7.9692° |
| perigee height: | 461 km |
| apogee height: | 35168 km |
| right ascension of ascending node: | 220.8249° |
| argument of perigee: | 155.1177° |
| revolutions per day: | 2.30714324 |
| mean anomaly at epoch: | 271.4014° |
| orbit number at epoch: | 19803 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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