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 22140.55088303 .00008630 00000-0 18856-3 0 9992
2 40354 74.7387 13.2660 0035887 207.6801 152.2504 15.43557347416292
| Epoch (UTC): | 20 May 2022 13:13:16 |
| Eccentricity: | 0.0035887 |
| inclination: | 74.7387° |
| perigee height: | 411 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 13.2660° |
| argument of perigee: | 207.6801° |
| revolutions per day: | 15.43557347 |
| mean anomaly at epoch: | 152.2504° |
| orbit number at epoch: | 41629 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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