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 26070U 00006B 24284.59151220 .00000416 00000-0 23633-3 0 9997
2 26070 71.0006 100.8175 0018640 248.7775 111.1357 14.15691037275653
| Epoch (UTC): | 10 October 2024 14:11:46 |
| Eccentricity: | 0.0018640 |
| inclination: | 71.0006° |
| perigee height: | 826 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 100.8175° |
| argument of perigee: | 248.7775° |
| revolutions per day: | 14.15691037 |
| mean anomaly at epoch: | 111.1357° |
| orbit number at epoch: | 27565 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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