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 23157.13698595 -.00000020 00000-0 40076-4 0 9999
2 36095 67.1488 64.7971 0008813 258.2763 101.7333 13.96839888690507
| Epoch (UTC): | 06 June 2023 03:17:15 |
| Eccentricity: | 0.0008813 |
| inclination: | 67.1488° |
| perigee height: | 898 km |
| apogee height: | 911 km |
| right ascension of ascending node: | 64.7971° |
| argument of perigee: | 258.2763° |
| revolutions per day: | 13.96839888 |
| mean anomaly at epoch: | 101.7333° |
| orbit number at epoch: | 69050 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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