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 23081.04640433 .00048045 00000-0 10632-2 0 9992
2 43937 97.0992 109.8456 0014194 226.3292 133.6781 15.43550694232561
| Epoch (UTC): | 22 March 2023 01:06:49 |
| Eccentricity: | 0.0014194 |
| inclination: | 97.0992° |
| perigee height: | 426 km |
| apogee height: | 445 km |
| right ascension of ascending node: | 109.8456° |
| argument of perigee: | 226.3292° |
| revolutions per day: | 15.43550694 |
| mean anomaly at epoch: | 133.6781° |
| orbit number at epoch: | 23256 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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