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 43196U 18015E 24283.56674783 .07825702 26886-5 28016-3 0 9999
2 43196 97.5747 108.8545 0010089 257.9555 102.0615 16.43491331373587
| Epoch (UTC): | 09 October 2024 13:36:07 |
| Eccentricity: | 0.0010089 |
| inclination: | 97.5747° |
| perigee height: | 150 km |
| apogee height: | 163 km |
| right ascension of ascending node: | 108.8545° |
| argument of perigee: | 257.9555° |
| revolutions per day: | 16.43491331 |
| mean anomaly at epoch: | 102.0615° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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