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 22178.56280487 .00009956 00000-0 33306-3 0 9996
2 43937 97.1293 211.5206 0022529 116.4025 243.9533 15.30915631191526
| Epoch (UTC): | 27 June 2022 13:30:26 |
| Eccentricity: | 0.0022529 |
| inclination: | 97.1293° |
| perigee height: | 457 km |
| apogee height: | 488 km |
| right ascension of ascending node: | 211.5206° |
| argument of perigee: | 116.4025° |
| revolutions per day: | 15.30915631 |
| mean anomaly at epoch: | 243.9533° |
| orbit number at epoch: | 19152 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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