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 43943U 26145.60586584 +.00000000 +00000-0 +21369-3 0 00000
2 43943 97.4724 240.7668 0003175 141.0863 219.0601 15.20278837 02
| Epoch (UTC): | 25 May 2026 14:32:26 |
| Eccentricity: | 0.0003175 |
| inclination: | 97.4724° |
| perigee height: | 503 km |
| apogee height: | 507 km |
| right ascension of ascending node: | 240.7668° |
| argument of perigee: | 141.0863° |
| revolutions per day: | 15.20278837 |
| mean anomaly at epoch: | 219.0601° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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