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 23153.77172909 .00000085 00000-0 11523-3 0 9995
2 36095 67.1487 72.9784 0008840 258.8202 101.1888 13.96840053690227
| Epoch (UTC): | 02 June 2023 18:31:17 |
| Eccentricity: | 0.0008840 |
| inclination: | 67.1487° |
| perigee height: | 898 km |
| apogee height: | 911 km |
| right ascension of ascending node: | 72.9784° |
| argument of perigee: | 258.8202° |
| revolutions per day: | 13.96840053 |
| mean anomaly at epoch: | 101.1888° |
| orbit number at epoch: | 69022 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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