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 23081.20986154 .00562265 00000-0 24250-2 0 9995
2 43131 97.3321 170.3575 0004730 278.2598 81.8135 15.83553678289536
| Epoch (UTC): | 22 March 2023 05:02:12 |
| Eccentricity: | 0.0004730 |
| inclination: | 97.3321° |
| perigee height: | 317 km |
| apogee height: | 323 km |
| right ascension of ascending node: | 170.3575° |
| argument of perigee: | 278.2598° |
| revolutions per day: | 15.83553678 |
| mean anomaly at epoch: | 81.8135° |
| orbit number at epoch: | 28953 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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