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 26061U 00004A 23266.40066907 .00001427 00000-0 44561-3 0 9997
2 26061 100.2159 58.1523 0033091 195.8674 164.1476 14.42491652242932
| Epoch (UTC): | 23 September 2023 09:36:57 |
| Eccentricity: | 0.0033091 |
| inclination: | 100.2159° |
| perigee height: | 726 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 58.1523° |
| argument of perigee: | 195.8674° |
| revolutions per day: | 14.42491652 |
| mean anomaly at epoch: | 164.1476° |
| orbit number at epoch: | 24293 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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