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 43937U 19003F 22135.60554794 .00016809 00000-0 58044-3 0 9990
2 43937 97.1331 170.2474 0018893 269.9395 89.9681 15.29840769184958
| Epoch (UTC): | 15 May 2022 14:31:59 |
| Eccentricity: | 0.0018893 |
| inclination: | 97.1331° |
| perigee height: | 463 km |
| apogee height: | 489 km |
| right ascension of ascending node: | 170.2474° |
| argument of perigee: | 269.9395° |
| revolutions per day: | 15.29840769 |
| mean anomaly at epoch: | 89.9681° |
| orbit number at epoch: | 18495 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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