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 39136U 13015G 23080.95740153 .00035991 00000-0 10964-2 0 9998
2 39136 64.8688 278.5375 0025691 279.6577 80.1655 15.33479658548752
| Epoch (UTC): | 21 March 2023 22:58:39 |
| Eccentricity: | 0.0025691 |
| inclination: | 64.8688° |
| perigee height: | 448 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 278.5375° |
| argument of perigee: | 279.6577° |
| revolutions per day: | 15.33479658 |
| mean anomaly at epoch: | 80.1655° |
| orbit number at epoch: | 54875 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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