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 23154.77414624 .00000024 00000-0 71398-4 0 9999
2 36095 67.1488 70.5415 0008842 258.7931 101.2160 13.96839864690360
| Epoch (UTC): | 03 June 2023 18:34:46 |
| Eccentricity: | 0.0008842 |
| inclination: | 67.1488° |
| perigee height: | 898 km |
| apogee height: | 911 km |
| right ascension of ascending node: | 70.5415° |
| argument of perigee: | 258.7931° |
| revolutions per day: | 13.96839864 |
| mean anomaly at epoch: | 101.2160° |
| orbit number at epoch: | 69036 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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