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 40354U 14084B 22149.17098505 .00006463 00000-0 14105-3 0 9999
2 40354 74.7379 355.3388 0035239 185.8659 174.2148 15.43690623418025
| Epoch (UTC): | 29 May 2022 04:06:13 |
| Eccentricity: | 0.0035239 |
| inclination: | 74.7379° |
| perigee height: | 411 km |
| apogee height: | 459 km |
| right ascension of ascending node: | 355.3388° |
| argument of perigee: | 185.8659° |
| revolutions per day: | 15.43690623 |
| mean anomaly at epoch: | 174.2148° |
| orbit number at epoch: | 41802 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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