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 43450U 26145.63874174 +.00000000 +00000-0 +00000-0 0 00007
2 43450 0.0294 334.6648 0001756 20.3857 252.1173 1.00273352 05
| Epoch (UTC): | 25 May 2026 15:19:47 |
| Eccentricity: | 0.0001756 |
| inclination: | 0.0294° |
| perigee height: | 35779 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 334.6648° |
| argument of perigee: | 20.3857° |
| revolutions per day: | 1.00273352 |
| mean anomaly at epoch: | 252.1173° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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