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 43131U 18004W 23090.20764167 .01363757 10000-2 28689-2 0 9992
2 43131 97.3224 180.0712 0008902 280.9751 79.0525 15.99058860290966
| Epoch (UTC): | 31 March 2023 04:59:00 |
| Eccentricity: | 0.0008902 |
| inclination: | 97.3224° |
| perigee height: | 271 km |
| apogee height: | 283 km |
| right ascension of ascending node: | 180.0712° |
| argument of perigee: | 280.9751° |
| revolutions per day: | 15.99058860 |
| mean anomaly at epoch: | 79.0525° |
| orbit number at epoch: | 29096 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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