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 08826U 71120C 24276.93062147 .00019887 00000-0 32193-2 0 9991
2 08826 81.2291 258.6908 0008478 240.5312 119.5047 14.71162039758327
| Epoch (UTC): | 02 October 2024 22:20:05 |
| Eccentricity: | 0.0008478 |
| inclination: | 81.2291° |
| perigee height: | 651 km |
| apogee height: | 663 km |
| right ascension of ascending node: | 258.6908° |
| argument of perigee: | 240.5312° |
| revolutions per day: | 14.71162039 |
| mean anomaly at epoch: | 119.5047° |
| orbit number at epoch: | 75832 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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