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 28352U 04021A 23333.83975768 .00000074 00000-0 66115-4 0 9998
2 28352 71.0001 243.3555 0014217 136.5610 223.6633 14.11843571 3435
| Epoch (UTC): | 29 November 2023 20:09:15 |
| Eccentricity: | 0.0014217 |
| inclination: | 71.0001° |
| perigee height: | 843 km |
| apogee height: | 863 km |
| right ascension of ascending node: | 243.3555° |
| argument of perigee: | 136.5610° |
| revolutions per day: | 14.11843571 |
| mean anomaly at epoch: | 223.6633° |
| orbit number at epoch: | 343 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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