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 25340.68159409 -.00000130 00000-0 -42978-4 0 9994
2 28353 71.0022 67.6780 0005627 209.1025 150.9784 14.14582233109689
| Epoch (UTC): | 06 December 2025 16:21:29 |
| Eccentricity: | 0.0005627 |
| inclination: | 71.0022° |
| perigee height: | 839 km |
| apogee height: | 848 km |
| right ascension of ascending node: | 67.6780° |
| argument of perigee: | 209.1025° |
| revolutions per day: | 14.14582233 |
| mean anomaly at epoch: | 150.9784° |
| orbit number at epoch: | 10968 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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