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 23091.93311054 .00058582 00000-0 12394-2 0 9999
2 43937 97.0979 120.4764 0015598 185.6919 174.4156 15.44810086234240
| Epoch (UTC): | 01 April 2023 22:23:40 |
| Eccentricity: | 0.0015598 |
| inclination: | 97.0979° |
| perigee height: | 421 km |
| apogee height: | 442 km |
| right ascension of ascending node: | 120.4764° |
| argument of perigee: | 185.6919° |
| revolutions per day: | 15.44810086 |
| mean anomaly at epoch: | 174.4156° |
| orbit number at epoch: | 23424 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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