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 42809U 17039G 23334.69243907 .00000035 00000-0 52701-5 0 9996
2 42809 86.3992 22.0871 0002028 104.0837 256.0584 14.34216597336731
| Epoch (UTC): | 30 November 2023 16:37:06 |
| Eccentricity: | 0.0002028 |
| inclination: | 86.3992° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 22.0871° |
| argument of perigee: | 104.0837° |
| revolutions per day: | 14.34216597 |
| mean anomaly at epoch: | 256.0584° |
| orbit number at epoch: | 33673 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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