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 26041.85941726 +.00000000 +00000-0 +63643-4 0 00007
2 36095 67.1466 200.1242 0007176 247.5069 112.5257 13.97037609 08
| Epoch (UTC): | 10 February 2026 20:37:33 |
| Eccentricity: | 0.0007176 |
| inclination: | 67.1466° |
| perigee height: | 899 km |
| apogee height: | 909 km |
| right ascension of ascending node: | 200.1242° |
| argument of perigee: | 247.5069° |
| revolutions per day: | 13.97037609 |
| mean anomaly at epoch: | 112.5257° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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