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 24256.17113577 .00000185 00000-0 18663-3 0 9993
2 36095 67.1503 16.5924 0008827 256.6169 103.3932 13.96931630755508
| Epoch (UTC): | 12 September 2024 04:06:26 |
| Eccentricity: | 0.0008827 |
| inclination: | 67.1503° |
| perigee height: | 898 km |
| apogee height: | 911 km |
| right ascension of ascending node: | 16.5924° |
| argument of perigee: | 256.6169° |
| revolutions per day: | 13.96931630 |
| mean anomaly at epoch: | 103.3932° |
| orbit number at epoch: | 75550 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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