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 43028U 26145.16100911 +.00000000 +00000-0 +18335-3 0 00000
2 43028 34.9955 50.8917 0000905 120.7045 239.3753 15.02680444 03
| Epoch (UTC): | 25 May 2026 03:51:51 |
| Eccentricity: | 0.0000905 |
| inclination: | 34.9955° |
| perigee height: | 558 km |
| apogee height: | 559 km |
| right ascension of ascending node: | 50.8917° |
| argument of perigee: | 120.7045° |
| revolutions per day: | 15.02680444 |
| mean anomaly at epoch: | 239.3753° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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