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 28352U 04021A 25200.89921932 .00000354 00000-0 21860-3 0 9991
2 28352 71.0051 73.8410 0010899 265.5835 94.4041 14.12118652 87806
| Epoch (UTC): | 19 July 2025 21:34:52 |
| Eccentricity: | 0.0010899 |
| inclination: | 71.0051° |
| perigee height: | 844 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 73.8410° |
| argument of perigee: | 265.5835° |
| revolutions per day: | 14.12118652 |
| mean anomaly at epoch: | 94.4041° |
| orbit number at epoch: | 8780 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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