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 22565U 93016A 23266.43960032 .00000145 00000-0 10490-3 0 9992
2 22565 70.8183 260.7945 0008505 284.0480 75.9694 14.12459119572467
| Epoch (UTC): | 23 September 2023 10:33:01 |
| Eccentricity: | 0.0008505 |
| inclination: | 70.8183° |
| perigee height: | 845 km |
| apogee height: | 857 km |
| right ascension of ascending node: | 260.7945° |
| argument of perigee: | 284.0480° |
| revolutions per day: | 14.12459119 |
| mean anomaly at epoch: | 75.9694° |
| orbit number at epoch: | 57246 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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