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 is defined by the following mean orbital elements,
1 26411U 00041B 24252.84969984 .00055454 -32453-3 00000+0 0 9994
2 26411 150.0714 39.2512 9137785 255.7698 0.1508 0.44419796 28488
| Epoch (UTC): | 08 September 2024 20:23:34 |
| Eccentricity: | 0.9137785 |
| inclination: | 150.0714° |
| perigee height: | -122 km |
| apogee height: | 132480 km |
| right ascension of ascending node: | 39.2512° |
| argument of perigee: | 255.7698° |
| revolutions per day: | 0.44419796 |
| mean anomaly at epoch: | 0.1508° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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