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 40024U 14033Q 22178.54079737 .00001937 00000-0 19781-3 0 9992
2 40024 97.9860 122.2419 0012591 21.8084 338.3667 14.91769181435480
| Epoch (UTC): | 27 June 2022 12:58:44 |
| Eccentricity: | 0.0012591 |
| inclination: | 97.9860° |
| perigee height: | 583 km |
| apogee height: | 601 km |
| right ascension of ascending node: | 122.2419° |
| argument of perigee: | 21.8084° |
| revolutions per day: | 14.91769181 |
| mean anomaly at epoch: | 338.3667° |
| orbit number at epoch: | 43548 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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