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 26145.45125014 +.00000000 +00000-0 +44794-4 0 00008
2 36095 67.1482 308.1926 0003668 253.2846 106.7837 13.97048537 04
| Epoch (UTC): | 25 May 2026 10:49:48 |
| Eccentricity: | 0.0003668 |
| inclination: | 67.1482° |
| perigee height: | 901 km |
| apogee height: | 907 km |
| right ascension of ascending node: | 308.1926° |
| argument of perigee: | 253.2846° |
| revolutions per day: | 13.97048537 |
| mean anomaly at epoch: | 106.7837° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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