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 00046U 60007B 25165.36806251 .00000474 00000-0 10754-3 0 9998
2 00046 66.6868 150.3178 0201166 211.5815 147.3098 14.53999449403518
| Epoch (UTC): | 14 June 2025 08:50:00 |
| Eccentricity: | 0.0201166 |
| inclination: | 66.6868° |
| perigee height: | 570 km |
| apogee height: | 855 km |
| right ascension of ascending node: | 150.3178° |
| argument of perigee: | 211.5815° |
| revolutions per day: | 14.53999449 |
| mean anomaly at epoch: | 147.3098° |
| orbit number at epoch: | 40351 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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