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 43677U 26050.45966639 +.00000000 +00000-0 +25501-3 0 00007
2 43677 98.0771 237.8836 0010087 151.0645 209.1140 15.02328710 02
| Epoch (UTC): | 19 February 2026 11:01:55 |
| Eccentricity: | 0.0010087 |
| inclination: | 98.0771° |
| perigee height: | 553 km |
| apogee height: | 567 km |
| right ascension of ascending node: | 237.8836° |
| argument of perigee: | 151.0645° |
| revolutions per day: | 15.02328710 |
| mean anomaly at epoch: | 209.1140° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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