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 43698U 26145.59464847 +.00000000 +00000-0 +00000-0 0 00008
2 43698 0.0108 284.8902 0003536 130.8708 96.5754 1.00273904 00
| Epoch (UTC): | 25 May 2026 14:16:17 |
| Eccentricity: | 0.0003536 |
| inclination: | 0.0108° |
| perigee height: | 35771 km |
| apogee height: | 35801 km |
| right ascension of ascending node: | 284.8902° |
| argument of perigee: | 130.8708° |
| revolutions per day: | 1.00273904 |
| mean anomaly at epoch: | 96.5754° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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