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 23147.82882691 -.00000008 00000-0 48156-4 0 9999
2 36095 67.1477 87.4256 0008989 260.7183 99.2885 13.96837835689399
| Epoch (UTC): | 27 May 2023 19:53:30 |
| Eccentricity: | 0.0008989 |
| inclination: | 67.1477° |
| perigee height: | 898 km |
| apogee height: | 911 km |
| right ascension of ascending node: | 87.4256° |
| argument of perigee: | 260.7183° |
| revolutions per day: | 13.96837835 |
| mean anomaly at epoch: | 99.2885° |
| orbit number at epoch: | 68939 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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