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 04363U 26031.77618088 +.00000000 +00000-0 +28474-4 0 00005
2 04363 99.8928 307.4591 0001775 352.5939 76.1366 13.46692807 03
| Epoch (UTC): | 31 January 2026 18:37:42 |
| Eccentricity: | 0.0001775 |
| inclination: | 99.8928° |
| perigee height: | 1083 km |
| apogee height: | 1086 km |
| right ascension of ascending node: | 307.4591° |
| argument of perigee: | 352.5939° |
| revolutions per day: | 13.46692807 |
| mean anomaly at epoch: | 76.1366° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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