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 04362U 26133.35354814 +.00000000 +00000-0 +13670-4 0 00007
2 04362 99.9621 54.7871 0008274 82.7530 31.1699 13.44753755 04
| Epoch (UTC): | 13 May 2026 08:29:06 |
| Eccentricity: | 0.0008274 |
| inclination: | 99.9621° |
| perigee height: | 1085 km |
| apogee height: | 1098 km |
| right ascension of ascending node: | 54.7871° |
| argument of perigee: | 82.7530° |
| revolutions per day: | 13.44753755 |
| mean anomaly at epoch: | 31.1699° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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