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 21938U 92020B 25188.48415213 .00000103 00000-0 91043-4 0 9993
2 21938 82.9317 335.8658 0027705 261.8508 158.8232 13.75513760667426
| Epoch (UTC): | 07 July 2025 11:37:10 |
| Eccentricity: | 0.0027705 |
| inclination: | 82.9317° |
| perigee height: | 959 km |
| apogee height: | 1000 km |
| right ascension of ascending node: | 335.8658° |
| argument of perigee: | 261.8508° |
| revolutions per day: | 13.75513760 |
| mean anomaly at epoch: | 158.8232° |
| orbit number at epoch: | 66742 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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