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 36869U 26162.03140890 +.00000000 +00000-0 +82307-3 0 00000
2 36869 20.1608 34.4815 4451277 186.4659 165.0307 6.62709859 09
| Epoch (UTC): | 11 June 2026 00:45:13 |
| Eccentricity: | 0.4451277 |
| inclination: | 20.1608° |
| perigee height: | 265 km |
| apogee height: | 10924 km |
| right ascension of ascending node: | 34.4815° |
| argument of perigee: | 186.4659° |
| revolutions per day: | 6.62709859 |
| mean anomaly at epoch: | 165.0307° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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