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 23087.19706012 .00803199 27131-3 23979-2 0 9990
2 43131 97.3269 176.7993 0007483 280.6652 79.3780 15.92372141290485
| Epoch (UTC): | 28 March 2023 04:43:45 |
| Eccentricity: | 0.0007483 |
| inclination: | 97.3269° |
| perigee height: | 290 km |
| apogee height: | 300 km |
| right ascension of ascending node: | 176.7993° |
| argument of perigee: | 280.6652° |
| revolutions per day: | 15.92372141 |
| mean anomaly at epoch: | 79.3780° |
| orbit number at epoch: | 29048 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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