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 28222U 04012C 24357.62891382 .00022549 00000-0 65443-3 0 9990
2 28222 97.7908 19.9802 0030422 106.2144 254.2449 15.35055609135914
| Epoch (UTC): | 22 December 2024 15:05:38 |
| Eccentricity: | 0.0030422 |
| inclination: | 97.7908° |
| perigee height: | 440 km |
| apogee height: | 481 km |
| right ascension of ascending node: | 19.9802° |
| argument of perigee: | 106.2144° |
| revolutions per day: | 15.35055609 |
| mean anomaly at epoch: | 254.2449° |
| orbit number at epoch: | 13591 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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