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 23333.97035063 -.00000172 00000-0 00000+0 0 9999
2 26609 6.0983 150.8834 7919023 225.6938 33.2233 1.25587719105968
| Epoch (UTC): | 29 November 2023 23:17:18 |
| Eccentricity: | 0.7919023 |
| inclination: | 6.0983° |
| perigee height: | 1173 km |
| apogee height: | 58647 km |
| right ascension of ascending node: | 150.8834° |
| argument of perigee: | 225.6938° |
| revolutions per day: | 1.25587719 |
| mean anomaly at epoch: | 33.2233° |
| orbit number at epoch: | 10596 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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