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 28367U 26017.94472898 +.00000000 +00000-0 +44153-4 0 00007
2 28367 98.1906 353.4625 0348415 299.5983 120.6918 13.88610101 05
| Epoch (UTC): | 17 January 2026 22:40:24 |
| Eccentricity: | 0.0348415 |
| inclination: | 98.1906° |
| perigee height: | 679 km |
| apogee height: | 1188 km |
| right ascension of ascending node: | 353.4625° |
| argument of perigee: | 299.5983° |
| revolutions per day: | 13.88610101 |
| mean anomaly at epoch: | 120.6918° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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