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 43228U 26145.40113373 +.00000000 +00000-0 +00000-0 0 00002
2 43228 0.0487 44.8453 0006389 12.9598 299.5857 1.00270691 09
| Epoch (UTC): | 25 May 2026 09:37:37 |
| Eccentricity: | 0.0006389 |
| inclination: | 0.0487° |
| perigee height: | 35760 km |
| apogee height: | 35814 km |
| right ascension of ascending node: | 44.8453° |
| argument of perigee: | 12.9598° |
| revolutions per day: | 1.00270691 |
| mean anomaly at epoch: | 299.5857° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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