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 00011U 59001A 22274.34016586 .00000289 00000-0 13648-3 0 9991
2 00011 32.8758 156.1315 1467238 291.7341 53.3605 11.86173615374237
| Epoch (UTC): | 01 October 2022 08:09:50 |
| Eccentricity: | 0.1467238 |
| inclination: | 32.8758° |
| perigee height: | 552 km |
| apogee height: | 2935 km |
| right ascension of ascending node: | 156.1315° |
| argument of perigee: | 291.7341° |
| revolutions per day: | 11.86173615 |
| mean anomaly at epoch: | 53.3605° |
| orbit number at epoch: | 37423 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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