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 22182.74466944 .00009309 00000-0 26097-3 0 9992
2 43131 97.3754 262.0612 0004413 295.0684 65.0102 15.36808588248778
| Epoch (UTC): | 01 July 2022 17:52:19 |
| Eccentricity: | 0.0004413 |
| inclination: | 97.3754° |
| perigee height: | 452 km |
| apogee height: | 458 km |
| right ascension of ascending node: | 262.0612° |
| argument of perigee: | 295.0684° |
| revolutions per day: | 15.36808588 |
| mean anomaly at epoch: | 65.0102° |
| orbit number at epoch: | 24877 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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