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 25196.93864777 .00007186 00000-0 53180-3 0 9999
2 20692 63.2978 36.2422 0888975 78.2594 291.6690 13.59888085 58905
| Epoch (UTC): | 15 July 2025 22:31:39 |
| Eccentricity: | 0.0888975 |
| inclination: | 63.2978° |
| perigee height: | 377 km |
| apogee height: | 1695 km |
| right ascension of ascending node: | 36.2422° |
| argument of perigee: | 78.2594° |
| revolutions per day: | 13.59888085 |
| mean anomaly at epoch: | 291.6690° |
| orbit number at epoch: | 5890 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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