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 36095U 26162.56136806 +.00000000 +00000-0 +29623-4 0 00004
2 36095 67.1483 266.5810 0003427 262.5756 97.4939 13.97050241 04
| Epoch (UTC): | 11 June 2026 13:28:22 |
| Eccentricity: | 0.0003427 |
| inclination: | 67.1483° |
| perigee height: | 902 km |
| apogee height: | 907 km |
| right ascension of ascending node: | 266.5810° |
| argument of perigee: | 262.5756° |
| revolutions per day: | 13.97050241 |
| mean anomaly at epoch: | 97.4939° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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