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 23341.37316499 -.00000210 00000-0 -86076-4 0 9992
2 22284 70.9789 318.8495 0019824 207.1245 152.8843 14.13487058596410
| Epoch (UTC): | 07 December 2023 08:57:21 |
| Eccentricity: | 0.0019824 |
| inclination: | 70.9789° |
| perigee height: | 833 km |
| apogee height: | 862 km |
| right ascension of ascending node: | 318.8495° |
| argument of perigee: | 207.1245° |
| revolutions per day: | 14.13487058 |
| mean anomaly at epoch: | 152.8843° |
| orbit number at epoch: | 59641 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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