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 43897U 18111X 22280.20041597 .00006336 00000-0 23932-3 0 9995
2 43897 97.1685 161.0569 0022917 53.0185 45.8464 15.27088898210280
| Epoch (UTC): | 07 October 2022 04:48:35 |
| Eccentricity: | 0.0022917 |
| inclination: | 97.1685° |
| perigee height: | 469 km |
| apogee height: | 500 km |
| right ascension of ascending node: | 161.0569° |
| argument of perigee: | 53.0185° |
| revolutions per day: | 15.27088898 |
| mean anomaly at epoch: | 45.8464° |
| orbit number at epoch: | 21028 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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