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 41460U 16025E 22277.07856810 .00031949 00000-0 11222-2 0 9990
2 41460 98.1826 97.8052 0116010 232.5290 126.5405 15.23072778354450
| Epoch (UTC): | 04 October 2022 01:53:08 |
| Eccentricity: | 0.0116010 |
| inclination: | 98.1826° |
| perigee height: | 417 km |
| apogee height: | 576 km |
| right ascension of ascending node: | 97.8052° |
| argument of perigee: | 232.5290° |
| revolutions per day: | 15.23072778 |
| mean anomaly at epoch: | 126.5405° |
| orbit number at epoch: | 35445 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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