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 22229.11225583 .00002249 00000-0 22757-3 0 9998
2 40024 97.9872 173.4849 0011157 200.3039 159.7737 14.91977295443545
| Epoch (UTC): | 17 August 2022 02:41:38 |
| Eccentricity: | 0.0011157 |
| inclination: | 97.9872° |
| perigee height: | 584 km |
| apogee height: | 599 km |
| right ascension of ascending node: | 173.4849° |
| argument of perigee: | 200.3039° |
| revolutions per day: | 14.91977295 |
| mean anomaly at epoch: | 159.7737° |
| orbit number at epoch: | 44354 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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