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 1328U 65032A 23337.61397409 -.00000004 00000-0 11988-3 0 9992
2 1328 41.1863 21.5997 0251225 167.3743 193.3452 13.38769143864572
| Epoch (UTC): | 03 December 2023 14:44:07 |
| Eccentricity: | 0.0251225 |
| inclination: | 41.1863° |
| perigee height: | 925 km |
| apogee height: | 1302 km |
| right ascension of ascending node: | 21.5997° |
| argument of perigee: | 167.3743° |
| revolutions per day: | 13.38769143 |
| mean anomaly at epoch: | 193.3452° |
| orbit number at epoch: | 86457 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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