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 26069U 00006A 23159.32265433 .00000392 00000-0 23300-3 0 9992
2 26069 70.9944 107.3759 0011120 172.7496 187.3788 14.13547779467806
| Epoch (UTC): | 08 June 2023 07:44:37 |
| Eccentricity: | 0.0011120 |
| inclination: | 70.9944° |
| perigee height: | 839 km |
| apogee height: | 855 km |
| right ascension of ascending node: | 107.3759° |
| argument of perigee: | 172.7496° |
| revolutions per day: | 14.13547779 |
| mean anomaly at epoch: | 187.3788° |
| orbit number at epoch: | 46780 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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