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 20104U 89050B 25196.90997180 .00000107 00000-0 91501-4 0 9993
2 20104 82.9579 141.4424 0042905 196.7306 163.2440 13.77581639810583
| Epoch (UTC): | 15 July 2025 21:50:21 |
| Eccentricity: | 0.0042905 |
| inclination: | 82.9579° |
| perigee height: | 941 km |
| apogee height: | 1004 km |
| right ascension of ascending node: | 141.4424° |
| argument of perigee: | 196.7306° |
| revolutions per day: | 13.77581639 |
| mean anomaly at epoch: | 163.2440° |
| orbit number at epoch: | 81058 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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