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 22719U 93046A 23272.49955685 .00000025 00000-0 00000-0 0 9997
2 22719 13.0426 21.0444 0005081 105.2041 282.4036 0.99049043 15370
| Epoch (UTC): | 29 September 2023 11:59:21 |
| Eccentricity: | 0.0005081 |
| inclination: | 13.0426° |
| perigee height: | 36111 km |
| apogee height: | 36154 km |
| right ascension of ascending node: | 21.0444° |
| argument of perigee: | 105.2041° |
| revolutions per day: | 0.99049043 |
| mean anomaly at epoch: | 282.4036° |
| orbit number at epoch: | 1537 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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