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 18986U 88023B 22176.93763719 .00000013 00000-0 -28206-5 0 9994
2 18986 82.9544 118.5440 0043081 106.1923 254.3983 13.78671253723163
| Epoch (UTC): | 25 June 2022 22:30:11 |
| Eccentricity: | 0.0043081 |
| inclination: | 82.9544° |
| perigee height: | 937 km |
| apogee height: | 1000 km |
| right ascension of ascending node: | 118.5440° |
| argument of perigee: | 106.1923° |
| revolutions per day: | 13.78671253 |
| mean anomaly at epoch: | 254.3983° |
| orbit number at epoch: | 72316 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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