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 39173U 13026B 23160.11129082 -.00000435 00000-0 00000-0 0 9994
2 39173 30.4303 40.9362 7642432 43.5607 355.9339 1.10512848 40040
| Epoch (UTC): | 09 June 2023 02:40:15 |
| Eccentricity: | 0.7642432 |
| inclination: | 30.4303° |
| perigee height: | 2938 km |
| apogee height: | 63340 km |
| right ascension of ascending node: | 40.9362° |
| argument of perigee: | 43.5607° |
| revolutions per day: | 1.10512848 |
| mean anomaly at epoch: | 355.9339° |
| orbit number at epoch: | 4004 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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