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 23085.75064834 .00731988 21548-3 24543-2 0 9999
2 43131 97.3286 175.2362 0006684 281.9204 78.1320 15.90093298290250
| Epoch (UTC): | 26 March 2023 18:00:56 |
| Eccentricity: | 0.0006684 |
| inclination: | 97.3286° |
| perigee height: | 297 km |
| apogee height: | 306 km |
| right ascension of ascending node: | 175.2362° |
| argument of perigee: | 281.9204° |
| revolutions per day: | 15.90093298 |
| mean anomaly at epoch: | 78.1320° |
| orbit number at epoch: | 29025 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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