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 00047U 60007C 22176.58089867 .00000351 00000-0 10399-3 0 9997
2 00047 66.6666 341.0719 0220627 124.3410 237.8788 14.42357916241112
| Epoch (UTC): | 25 June 2022 13:56:29 |
| Eccentricity: | 0.0220627 |
| inclination: | 66.6666° |
| perigee height: | 593 km |
| apogee height: | 908 km |
| right ascension of ascending node: | 341.0719° |
| argument of perigee: | 124.3410° |
| revolutions per day: | 14.42357916 |
| mean anomaly at epoch: | 237.8788° |
| orbit number at epoch: | 24111 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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