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 26382U 00032A 23342.30500503 .00000110 00000-0 00000-0 0 9998
2 26382 12.3604 23.3269 0000708 261.3310 123.2372 1.00079025 85709
| Epoch (UTC): | 08 December 2023 07:19:12 |
| Eccentricity: | 0.0000708 |
| inclination: | 12.3604° |
| perigee height: | 35837 km |
| apogee height: | 35843 km |
| right ascension of ascending node: | 23.3269° |
| argument of perigee: | 261.3310° |
| revolutions per day: | 1.00079025 |
| mean anomaly at epoch: | 123.2372° |
| orbit number at epoch: | 8570 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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