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 43743U 18096AA 23295.86021167 .15419510 25267-5 20216-3 0 9994
2 43743 97.2858 29.3911 0011730 268.5420 91.4540 16.48838571274250
| Epoch (UTC): | 22 October 2023 20:38:42 |
| Eccentricity: | 0.0011730 |
| inclination: | 97.2858° |
| perigee height: | 135 km |
| apogee height: | 150 km |
| right ascension of ascending node: | 29.3911° |
| argument of perigee: | 268.5420° |
| revolutions per day: | 16.48838571 |
| mean anomaly at epoch: | 91.4540° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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