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 is defined by the following mean orbital elements,
1 43937U 19003F 23313.54107761 .16492241 25339-5 26604-3 0 9999
2 43937 97.0315 342.1459 0005268 231.7168 128.3663 16.48231493268837
| Epoch (UTC): | 09 November 2023 12:59:09 |
| Eccentricity: | 0.0005268 |
| inclination: | 97.0315° |
| perigee height: | 140 km |
| apogee height: | 147 km |
| right ascension of ascending node: | 342.1459° |
| argument of perigee: | 231.7168° |
| revolutions per day: | 16.48231493 |
| mean anomaly at epoch: | 128.3663° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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