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 22327U 92093Q 23336.58868579 .00008070 00000-0 10030-2 0 9993
2 22327 71.1228 17.4354 0079737 132.6443 345.1673 14.80575353645688
| Epoch (UTC): | 02 December 2023 14:07:42 |
| Eccentricity: | 0.0079737 |
| inclination: | 71.1228° |
| perigee height: | 571 km |
| apogee height: | 683 km |
| right ascension of ascending node: | 17.4354° |
| argument of perigee: | 132.6443° |
| revolutions per day: | 14.80575353 |
| mean anomaly at epoch: | 345.1673° |
| orbit number at epoch: | 64568 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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