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 23090.70805126 .01483887 12621-2 28844-2 0 9999
2 43131 97.3210 180.6189 0009125 280.8035 79.2216 16.00526771291040
| Epoch (UTC): | 31 March 2023 16:59:35 |
| Eccentricity: | 0.0009125 |
| inclination: | 97.3210° |
| perigee height: | 267 km |
| apogee height: | 279 km |
| right ascension of ascending node: | 180.6189° |
| argument of perigee: | 280.8035° |
| revolutions per day: | 16.00526771 |
| mean anomaly at epoch: | 79.2216° |
| orbit number at epoch: | 29104 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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