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 26092U 00004K 23273.45534899 .00001647 00000-0 48421-3 0 9997
2 26092 100.2124 83.0607 0033759 105.7406 254.7506 14.45184215243064
| Epoch (UTC): | 30 September 2023 10:55:42 |
| Eccentricity: | 0.0033759 |
| inclination: | 100.2124° |
| perigee height: | 717 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 83.0607° |
| argument of perigee: | 105.7406° |
| revolutions per day: | 14.45184215 |
| mean anomaly at epoch: | 254.7506° |
| orbit number at epoch: | 24306 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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