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 43029U 26145.41534251 +.00000000 +00000-0 +18451-3 0 00006
2 43029 34.9948 49.0154 0002844 19.6983 340.3834 15.02561700 06
| Epoch (UTC): | 25 May 2026 09:58:05 |
| Eccentricity: | 0.0002844 |
| inclination: | 34.9948° |
| perigee height: | 557 km |
| apogee height: | 561 km |
| right ascension of ascending node: | 49.0154° |
| argument of perigee: | 19.6983° |
| revolutions per day: | 15.02561700 |
| mean anomaly at epoch: | 340.3834° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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