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 44543U 26144.33803472 +.00000000 +00000-0 +00000-0 0 00000
2 44543 54.3934 183.5003 0005463 340.7166 104.4121 1.86227242 02
| Epoch (UTC): | 24 May 2026 08:06:46 |
| Eccentricity: | 0.0005463 |
| inclination: | 54.3934° |
| perigee height: | 21513 km |
| apogee height: | 21544 km |
| right ascension of ascending node: | 183.5003° |
| argument of perigee: | 340.7166° |
| revolutions per day: | 1.86227242 |
| mean anomaly at epoch: | 104.4121° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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