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 43786U 26050.37740925 +.00000000 +00000-0 +33887-3 0 00003
2 43786 97.4203 104.2776 0014000 48.7475 311.4962 15.17350703 00
| Epoch (UTC): | 19 February 2026 09:03:28 |
| Eccentricity: | 0.0014000 |
| inclination: | 97.4203° |
| perigee height: | 504 km |
| apogee height: | 524 km |
| right ascension of ascending node: | 104.2776° |
| argument of perigee: | 48.7475° |
| revolutions per day: | 15.17350703 |
| mean anomaly at epoch: | 311.4962° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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