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 22287U 92094B 22145.62915869 .00000353 00000-0 45202-4 0 9993
2 22287 82.5256 199.8575 0024523 185.3274 174.7682 14.78281692563930
| Epoch (UTC): | 25 May 2022 15:05:59 |
| Eccentricity: | 0.0024523 |
| inclination: | 82.5256° |
| perigee height: | 617 km |
| apogee height: | 652 km |
| right ascension of ascending node: | 199.8575° |
| argument of perigee: | 185.3274° |
| revolutions per day: | 14.78281692 |
| mean anomaly at epoch: | 174.7682° |
| orbit number at epoch: | 56393 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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