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 25861U 99039B 23155.54243748 .00000567 00000-0 83441-4 0 9997
2 25861 98.1387 192.7027 0014004 280.9676 78.9960 14.79332484287545
| Epoch (UTC): | 04 June 2023 13:01:06 |
| Eccentricity: | 0.0014004 |
| inclination: | 98.1387° |
| perigee height: | 621 km |
| apogee height: | 641 km |
| right ascension of ascending node: | 192.7027° |
| argument of perigee: | 280.9676° |
| revolutions per day: | 14.79332484 |
| mean anomaly at epoch: | 78.9960° |
| orbit number at epoch: | 28754 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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