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 20666U 90055D 25196.75999223 .00001506 00000-0 12844-3 0 9992
2 20666 62.7841 338.6027 0022032 199.2528 160.7741 15.02126746902588
| Epoch (UTC): | 15 July 2025 18:14:23 |
| Eccentricity: | 0.0022032 |
| inclination: | 62.7841° |
| perigee height: | 545 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 338.6027° |
| argument of perigee: | 199.2528° |
| revolutions per day: | 15.02126746 |
| mean anomaly at epoch: | 160.7741° |
| orbit number at epoch: | 90258 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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