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 39120U 13011A 23080.67911201 -.00000272 00000-0 00000-0 0 9993
2 39120 2.2435 34.8034 0002238 319.4570 31.1324 1.00271294 36660
| Epoch (UTC): | 21 March 2023 16:17:55 |
| Eccentricity: | 0.0002238 |
| inclination: | 2.2435° |
| perigee height: | 35777 km |
| apogee height: | 35796 km |
| right ascension of ascending node: | 34.8034° |
| argument of perigee: | 319.4570° |
| revolutions per day: | 1.00271294 |
| mean anomaly at epoch: | 31.1324° |
| orbit number at epoch: | 3666 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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