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 26080U 00004H 24278.65414454 .00004552 00000-0 12925-2 0 9993
2 26080 100.1861 177.2645 0030709 141.8954 218.4411 14.45777309297172
| Epoch (UTC): | 04 October 2024 15:41:58 |
| Eccentricity: | 0.0030709 |
| inclination: | 100.1861° |
| perigee height: | 717 km |
| apogee height: | 761 km |
| right ascension of ascending node: | 177.2645° |
| argument of perigee: | 141.8954° |
| revolutions per day: | 14.45777309 |
| mean anomaly at epoch: | 218.4411° |
| orbit number at epoch: | 29717 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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