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 23027.39457859 .00000008 00000-0 59896-4 0 9994
2 36095 67.1485 20.2117 0007983 290.3357 69.6870 13.96815558672388
| Epoch (UTC): | 27 January 2023 09:28:11 |
| Eccentricity: | 0.0007983 |
| inclination: | 67.1485° |
| perigee height: | 899 km |
| apogee height: | 910 km |
| right ascension of ascending node: | 20.2117° |
| argument of perigee: | 290.3357° |
| revolutions per day: | 13.96815558 |
| mean anomaly at epoch: | 69.6870° |
| orbit number at epoch: | 67238 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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