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 43476U 18047A 26053.12578679 +.00005274 00000-0 +14423-3 0 03
2 43476 88.9879 213.7597 0011011 185.5928 253.3209 15.37245441432123
| Epoch (UTC): | 22 February 2026 03:01:07 |
| Eccentricity: | 0.0011011 |
| inclination: | 88.9879° |
| perigee height: | 447 km |
| apogee height: | 462 km |
| right ascension of ascending node: | 213.7597° |
| argument of perigee: | 185.5928° |
| revolutions per day: | 15.37245441 |
| mean anomaly at epoch: | 253.3209° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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