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 24278.15120333 .00000175 00000-0 17919-3 0 9995
2 36095 67.1490 323.1512 0008347 251.5620 108.4558 13.96939087758570
| Epoch (UTC): | 04 October 2024 03:37:43 |
| Eccentricity: | 0.0008347 |
| inclination: | 67.1490° |
| perigee height: | 898 km |
| apogee height: | 910 km |
| right ascension of ascending node: | 323.1512° |
| argument of perigee: | 251.5620° |
| revolutions per day: | 13.96939087 |
| mean anomaly at epoch: | 108.4558° |
| orbit number at epoch: | 75857 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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