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 25199.19976850 -.00000056 00000-0 -40988-5 0 9996
2 17974 71.0071 167.1894 0014902 211.2874 239.0540 14.17593393975091
| Epoch (UTC): | 18 July 2025 04:47:39 |
| Eccentricity: | 0.0014902 |
| inclination: | 71.0071° |
| perigee height: | 823 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 167.1894° |
| argument of perigee: | 211.2874° |
| revolutions per day: | 14.17593393 |
| mean anomaly at epoch: | 239.0540° |
| orbit number at epoch: | 97509 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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