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 28353U 04021B 25196.91972139 -.00000165 00000-0 -61089-4 0 9994
2 28353 71.0020 9.3556 0004216 11.2268 348.8947 14.14556955 89357
| Epoch (UTC): | 15 July 2025 22:04:23 |
| Eccentricity: | 0.0004216 |
| inclination: | 71.0020° |
| perigee height: | 841 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 9.3556° |
| argument of perigee: | 11.2268° |
| revolutions per day: | 14.14556955 |
| mean anomaly at epoch: | 348.8947° |
| orbit number at epoch: | 8935 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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