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 39206U 13036A 23273.55569802 .00000056 00000-0 00000+0 0 9990
2 39206 3.2179 35.9772 0058183 178.2330 177.8789 1.00274038 37378
| Epoch (UTC): | 30 September 2023 13:20:12 |
| Eccentricity: | 0.0058183 |
| inclination: | 3.2179° |
| perigee height: | 35540 km |
| apogee height: | 36031 km |
| right ascension of ascending node: | 35.9772° |
| argument of perigee: | 178.2330° |
| revolutions per day: | 1.00274038 |
| mean anomaly at epoch: | 177.8789° |
| orbit number at epoch: | 3737 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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