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 43775U 18099T 22135.93001023 .00002569 00000-0 23436-3 0 9997
2 43775 97.6225 203.2647 0014765 22.9149 337.2728 14.95885688188149
| Epoch (UTC): | 15 May 2022 22:19:12 |
| Eccentricity: | 0.0014765 |
| inclination: | 97.6225° |
| perigee height: | 569 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 203.2647° |
| argument of perigee: | 22.9149° |
| revolutions per day: | 14.95885688 |
| mean anomaly at epoch: | 337.2728° |
| orbit number at epoch: | 18814 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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