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 22227.77931341 -.00000070 00000-0 38170-5 0 9993
2 36095 67.1477 60.3901 0003343 258.6744 101.3965 13.96796600649398
| Epoch (UTC): | 15 August 2022 18:42:12 |
| Eccentricity: | 0.0003343 |
| inclination: | 67.1477° |
| perigee height: | 902 km |
| apogee height: | 907 km |
| right ascension of ascending node: | 60.3901° |
| argument of perigee: | 258.6744° |
| revolutions per day: | 13.96796600 |
| mean anomaly at epoch: | 101.3965° |
| orbit number at epoch: | 64939 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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