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 26065.62762727 +.00000000 +00000-0 +74365-4 0 00003
2 36095 67.1477 142.3243 0006474 244.9108 115.1305 13.97040448 01
| Epoch (UTC): | 06 March 2026 15:03:46 |
| Eccentricity: | 0.0006474 |
| inclination: | 67.1477° |
| perigee height: | 899 km |
| apogee height: | 909 km |
| right ascension of ascending node: | 142.3243° |
| argument of perigee: | 244.9108° |
| revolutions per day: | 13.97040448 |
| mean anomaly at epoch: | 115.1305° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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