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 17974U 87041B 23150.06714071 -.00000168 00000-0 -59275-4 0 9994
2 17974 71.0091 11.5081 0015530 309.2376 202.6956 14.17358899864304
| Epoch (UTC): | 30 May 2023 01:36:40 |
| Eccentricity: | 0.0015530 |
| inclination: | 71.0091° |
| perigee height: | 823 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 11.5081° |
| argument of perigee: | 309.2376° |
| revolutions per day: | 14.17358899 |
| mean anomaly at epoch: | 202.6956° |
| orbit number at epoch: | 86430 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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