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 35362U 26145.61711272 +.00000000 +00000-0 +00000-0 0 00007
2 35362 0.0328 27.2183 0002979 33.7823 204.3568 1.00271375 04
| Epoch (UTC): | 25 May 2026 14:48:38 |
| Eccentricity: | 0.0002979 |
| inclination: | 0.0328° |
| perigee height: | 35774 km |
| apogee height: | 35799 km |
| right ascension of ascending node: | 27.2183° |
| argument of perigee: | 33.7823° |
| revolutions per day: | 1.00271375 |
| mean anomaly at epoch: | 204.3568° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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