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 26105.57528904 +.00000000 +00000-0 +34957-5 0 00003
2 36095 67.1490 45.1690 0004965 244.2763 115.7809 13.97044906 03
| Epoch (UTC): | 15 April 2026 13:48:24 |
| Eccentricity: | 0.0004965 |
| inclination: | 67.1490° |
| perigee height: | 900 km |
| apogee height: | 908 km |
| right ascension of ascending node: | 45.1690° |
| argument of perigee: | 244.2763° |
| revolutions per day: | 13.97044906 |
| mean anomaly at epoch: | 115.7809° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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