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 24282.54242854 .00000591 00000-0 32520-3 0 9993
2 26070 71.0007 105.1258 0018657 251.3332 108.5766 14.15689649275369
| Epoch (UTC): | 08 October 2024 13:01:05 |
| Eccentricity: | 0.0018657 |
| inclination: | 71.0007° |
| perigee height: | 826 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 105.1258° |
| argument of perigee: | 251.3332° |
| revolutions per day: | 14.15689649 |
| mean anomaly at epoch: | 108.5766° |
| orbit number at epoch: | 27536 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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