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 26064U 00004D 23274.17899100 .00000294 00000-0 11952-3 0 9991
2 26064 100.1900 5.3416 0037197 331.8377 28.0791 14.36510850240825
| Epoch (UTC): | 01 October 2023 04:17:44 |
| Eccentricity: | 0.0037197 |
| inclination: | 100.1900° |
| perigee height: | 743 km |
| apogee height: | 796 km |
| right ascension of ascending node: | 5.3416° |
| argument of perigee: | 331.8377° |
| revolutions per day: | 14.36510850 |
| mean anomaly at epoch: | 28.0791° |
| orbit number at epoch: | 24082 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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