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 43039U 26145.43628009 +.00000000 +00000-0 +00000-0 0 00002
2 43039 0.0119 303.0677 0002601 106.9163 325.3173 1.00271335 09
| Epoch (UTC): | 25 May 2026 10:28:14 |
| Eccentricity: | 0.0002601 |
| inclination: | 0.0119° |
| perigee height: | 35776 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 303.0677° |
| argument of perigee: | 106.9163° |
| revolutions per day: | 1.00271335 |
| mean anomaly at epoch: | 325.3173° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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