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 43600U 18066A 23209.73257513 .24348956 20945-5 58706-4 0 9999
2 43600 96.7031 214.9023 0058712 264.1723 95.3504 16.56201943285581
| Epoch (UTC): | 28 July 2023 17:34:54 |
| Eccentricity: | 0.0058712 |
| inclination: | 96.7031° |
| perigee height: | 85 km |
| apogee height: | 161 km |
| right ascension of ascending node: | 214.9023° |
| argument of perigee: | 264.1723° |
| revolutions per day: | 16.56201943 |
| mean anomaly at epoch: | 95.3504° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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