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 is defined by the following mean orbital elements,
1 28096U 26022.28958604 +.00000000 +00000-0 +11468-3 0 00005
2 28096 63.6801 43.4611 0075246 122.8722 237.9576 13.41058482 03
| Epoch (UTC): | 22 January 2026 06:57:00 |
| Eccentricity: | 0.0075246 |
| inclination: | 63.6801° |
| perigee height: | 1049 km |
| apogee height: | 1162 km |
| right ascension of ascending node: | 43.4611° |
| argument of perigee: | 122.8722° |
| revolutions per day: | 13.41058482 |
| mean anomaly at epoch: | 237.9576° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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