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 26609U 00072B 21333.72585035 -.00000305 00000-0 00000-0 0 9998
2 26609 8.6878 301.7723 7973441 313.2948 3.3415 1.25588859 96642
| Epoch (UTC): | 29 November 2021 17:25:13 |
| Eccentricity: | 0.7973441 |
| inclination: | 8.6878° |
| perigee height: | 976 km |
| apogee height: | 58844 km |
| right ascension of ascending node: | 301.7723° |
| argument of perigee: | 313.2948° |
| revolutions per day: | 1.25588859 |
| mean anomaly at epoch: | 3.3415° |
| orbit number at epoch: | 9664 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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