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 20692U 90050D 25188.11401816 .00008827 00000-0 65177-3 0 9993
2 20692 63.2980 59.9357 0889225 78.0786 291.8439 13.59756029 57709
| Epoch (UTC): | 07 July 2025 02:44:11 |
| Eccentricity: | 0.0889225 |
| inclination: | 63.2980° |
| perigee height: | 377 km |
| apogee height: | 1696 km |
| right ascension of ascending node: | 59.9357° |
| argument of perigee: | 78.0786° |
| revolutions per day: | 13.59756029 |
| mean anomaly at epoch: | 291.8439° |
| orbit number at epoch: | 5770 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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