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 28541U 05004C 26011.20733487 0.00000001 00000-0 74809-6 0 01
2 28541 63.4183 110.9927 0546949 3.2202 356.6832 13.40658770 06
| Epoch (UTC): | 11 January 2026 04:58:33 |
| Eccentricity: | 0.0546949 |
| inclination: | 63.4183° |
| perigee height: | 697 km |
| apogee height: | 1516 km |
| right ascension of ascending node: | 110.9927° |
| argument of perigee: | 3.2202° |
| revolutions per day: | 13.40658770 |
| mean anomaly at epoch: | 356.6832° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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