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 22698U 93041A 23081.19013335 .00000215 00000-0 84621-4 0 9996
2 22698 89.5218 127.5594 0091157 95.6428 265.5167 14.23584639544125
| Epoch (UTC): | 22 March 2023 04:33:47 |
| Eccentricity: | 0.0091157 |
| inclination: | 89.5218° |
| perigee height: | 748 km |
| apogee height: | 879 km |
| right ascension of ascending node: | 127.5594° |
| argument of perigee: | 95.6428° |
| revolutions per day: | 14.23584639 |
| mean anomaly at epoch: | 265.5167° |
| orbit number at epoch: | 54412 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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