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 data is extracted from the following two-line orbital elements,
1 36095U 09063A 23153.19891939 .00000084 00000-0 11455-3 0 9995
2 36095 67.1486 74.3709 0008887 259.1112 100.8973 13.96839885690147
| Epoch (UTC): | 02 June 2023 04:46:26 |
| Eccentricity: | 0.0008887 |
| inclination: | 67.1486° |
| perigee height: | 898 km |
| apogee height: | 911 km |
| right ascension of ascending node: | 74.3709° |
| argument of perigee: | 259.1112° |
| revolutions per day: | 13.96839885 |
| mean anomaly at epoch: | 100.8973° |
| orbit number at epoch: | 69014 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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