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 23152.20003496 -.00000115 00000-0 -34326-4 0 9999
2 26070 71.0038 66.2941 0018927 281.4226 78.4771 14.15550005205249
| Epoch (UTC): | 01 June 2023 04:48:03 |
| Eccentricity: | 0.0018927 |
| inclination: | 71.0038° |
| perigee height: | 827 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 66.2941° |
| argument of perigee: | 281.4226° |
| revolutions per day: | 14.15550005 |
| mean anomaly at epoch: | 78.4771° |
| orbit number at epoch: | 20524 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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