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 06392U 26088.16882450 +.00000000 +00000-0 +15449-3 0 00007
2 06392 81.2415 5.7962 0055457 65.1076 295.5844 14.08100693 02
| Epoch (UTC): | 29 March 2026 04:03:06 |
| Eccentricity: | 0.0055457 |
| inclination: | 81.2415° |
| perigee height: | 826 km |
| apogee height: | 906 km |
| right ascension of ascending node: | 5.7962° |
| argument of perigee: | 65.1076° |
| revolutions per day: | 14.08100693 |
| mean anomaly at epoch: | 295.5844° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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