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 22284U 92093A 23151.99396463 -.00000221 00000-0 -92279-4 0 9992
2 22284 70.9793 355.9790 0016576 130.2062 230.0514 14.13436342569929
| Epoch (UTC): | 31 May 2023 23:51:18 |
| Eccentricity: | 0.0016576 |
| inclination: | 70.9793° |
| perigee height: | 835 km |
| apogee height: | 859 km |
| right ascension of ascending node: | 355.9790° |
| argument of perigee: | 130.2062° |
| revolutions per day: | 14.13436342 |
| mean anomaly at epoch: | 230.0514° |
| orbit number at epoch: | 56992 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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