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 25198.13658716 .00000355 00000-0 21923-3 0 9992
2 28352 71.0050 79.6140 0010891 268.9095 91.0778 14.12116326 87419
| Epoch (UTC): | 17 July 2025 03:16:41 |
| Eccentricity: | 0.0010891 |
| inclination: | 71.0050° |
| perigee height: | 844 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 79.6140° |
| argument of perigee: | 268.9095° |
| revolutions per day: | 14.12116326 |
| mean anomaly at epoch: | 91.0778° |
| orbit number at epoch: | 8741 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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