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 41915U 17002C 22280.09152556 .00006732 00000-0 36693-3 0 9995
2 41915 97.2840 322.1027 0007871 246.0619 197.8968 15.14679448316782
| Epoch (UTC): | 07 October 2022 02:11:47 |
| Eccentricity: | 0.0007871 |
| inclination: | 97.2840° |
| perigee height: | 516 km |
| apogee height: | 527 km |
| right ascension of ascending node: | 322.1027° |
| argument of perigee: | 246.0619° |
| revolutions per day: | 15.14679448 |
| mean anomaly at epoch: | 197.8968° |
| orbit number at epoch: | 31678 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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