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 is defined by the following mean orbital elements,
1 43679U 26145.38173933 +.00000000 +00000-0 +28248-3 0 00004
2 43679 98.0531 357.9497 0001067 200.8011 159.3177 15.16756583 07
| Epoch (UTC): | 25 May 2026 09:09:42 |
| Eccentricity: | 0.0001067 |
| inclination: | 98.0531° |
| perigee height: | 515 km |
| apogee height: | 516 km |
| right ascension of ascending node: | 357.9497° |
| argument of perigee: | 200.8011° |
| revolutions per day: | 15.16756583 |
| mean anomaly at epoch: | 159.3177° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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