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 43155U 18008A 24235.75891043 .18791616 24620-5 29649-3 0 9999
2 43155 97.1927 292.6688 0013149 268.0079 91.9719 16.47546330365397
| Epoch (UTC): | 22 August 2024 18:12:49 |
| Eccentricity: | 0.0013149 |
| inclination: | 97.1927° |
| perigee height: | 137 km |
| apogee height: | 154 km |
| right ascension of ascending node: | 292.6688° |
| argument of perigee: | 268.0079° |
| revolutions per day: | 16.47546330 |
| mean anomaly at epoch: | 91.9719° |
| orbit number at epoch: | 36539 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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