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 39026U 12072A 23086.93010940 .00067723 00000-0 10209-2 0 9996
2 39026 97.2844 82.1981 0019180 200.5514 159.4971 15.54347732572620
| Epoch (UTC): | 27 March 2023 22:19:21 |
| Eccentricity: | 0.0019180 |
| inclination: | 97.2844° |
| perigee height: | 391 km |
| apogee height: | 417 km |
| right ascension of ascending node: | 82.1981° |
| argument of perigee: | 200.5514° |
| revolutions per day: | 15.54347732 |
| mean anomaly at epoch: | 159.4971° |
| orbit number at epoch: | 57262 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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