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 43910U 26145.60602669 +.00000000 +00000-0 +12995-3 0 00002
2 43910 50.0099 203.7053 0004949 149.7094 210.4108 14.29004515 09
| Epoch (UTC): | 25 May 2026 14:32:40 |
| Eccentricity: | 0.0004949 |
| inclination: | 50.0099° |
| perigee height: | 792 km |
| apogee height: | 799 km |
| right ascension of ascending node: | 203.7053° |
| argument of perigee: | 149.7094° |
| revolutions per day: | 14.29004515 |
| mean anomaly at epoch: | 210.4108° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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