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 26157.04890583 +.00000000 +00000-0 +50675-4 0 00001
2 36095 67.1486 279.9866 0003458 259.1529 100.9167 13.97049739 03
| Epoch (UTC): | 06 June 2026 01:10:25 |
| Eccentricity: | 0.0003458 |
| inclination: | 67.1486° |
| perigee height: | 902 km |
| apogee height: | 907 km |
| right ascension of ascending node: | 279.9866° |
| argument of perigee: | 259.1529° |
| revolutions per day: | 13.97049739 |
| mean anomaly at epoch: | 100.9167° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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