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 22227.39618106 -.00000207 00000-0 -81438-4 0 9999
2 26070 71.0039 315.3487 0016766 355.5443 4.5528 14.15496125164253
| Epoch (UTC): | 15 August 2022 09:30:30 |
| Eccentricity: | 0.0016766 |
| inclination: | 71.0039° |
| perigee height: | 828 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 315.3487° |
| argument of perigee: | 355.5443° |
| revolutions per day: | 14.15496125 |
| mean anomaly at epoch: | 4.5528° |
| orbit number at epoch: | 16425 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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