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 00050U 60009B 25189.21955452 -.00000105 00000-0 -17673-3 0 9993
2 00050 47.2286 149.3799 0112922 69.4316 291.8547 12.20156568895705
| Epoch (UTC): | 08 July 2025 05:16:09 |
| Eccentricity: | 0.0112922 |
| inclination: | 47.2286° |
| perigee height: | 1502 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 149.3799° |
| argument of perigee: | 69.4316° |
| revolutions per day: | 12.20156568 |
| mean anomaly at epoch: | 291.8547° |
| orbit number at epoch: | 89570 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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