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 43819U 26145.56105169 +.00000000 +00000-0 +11997-3 0 00009
2 43819 97.3983 185.2231 0020069 71.0682 289.2719 15.06388661 01
| Epoch (UTC): | 25 May 2026 13:27:54 |
| Eccentricity: | 0.0020069 |
| inclination: | 97.3983° |
| perigee height: | 533 km |
| apogee height: | 561 km |
| right ascension of ascending node: | 185.2231° |
| argument of perigee: | 71.0682° |
| revolutions per day: | 15.06388661 |
| mean anomaly at epoch: | 289.2719° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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