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 23080.00911772 .00049111 00000-0 10904-2 0 9991
2 43937 97.0995 108.8337 0014058 230.5718 129.4287 15.43449116232403
| Epoch (UTC): | 21 March 2023 00:13:07 |
| Eccentricity: | 0.0014058 |
| inclination: | 97.0995° |
| perigee height: | 426 km |
| apogee height: | 445 km |
| right ascension of ascending node: | 108.8337° |
| argument of perigee: | 230.5718° |
| revolutions per day: | 15.43449116 |
| mean anomaly at epoch: | 129.4287° |
| orbit number at epoch: | 23240 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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