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 04327U 26133.36132911 +.00000000 +00000-0 +21698-4 0 00000
2 04327 99.2831 72.9460 0005088 11.2706 99.0564 13.58736889 07
| Epoch (UTC): | 13 May 2026 08:40:18 |
| Eccentricity: | 0.0005088 |
| inclination: | 99.2831° |
| perigee height: | 1037 km |
| apogee height: | 1044 km |
| right ascension of ascending node: | 72.9460° |
| argument of perigee: | 11.2706° |
| revolutions per day: | 13.58736889 |
| mean anomaly at epoch: | 99.0564° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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