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 26068.49126323 +.00000000 +00000-0 +39071-4 0 00002
2 36095 67.1475 135.3605 0006413 244.9358 115.1061 13.97040803 07
| Epoch (UTC): | 09 March 2026 11:47:25 |
| Eccentricity: | 0.0006413 |
| inclination: | 67.1475° |
| perigee height: | 899 km |
| apogee height: | 909 km |
| right ascension of ascending node: | 135.3605° |
| argument of perigee: | 244.9358° |
| revolutions per day: | 13.97040803 |
| mean anomaly at epoch: | 115.1061° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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