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 44344U 26108.34351788 +.00000000 +00000-0 +00000-0 0 00008
2 44344 42.3256 12.5475 1968355 350.1672 6.5248 4.54376217 02
| Epoch (UTC): | 18 April 2026 08:14:39 |
| Eccentricity: | 0.1968355 |
| inclination: | 42.3256° |
| perigee height: | 5989 km |
| apogee height: | 12050 km |
| right ascension of ascending node: | 12.5475° |
| argument of perigee: | 350.1672° |
| revolutions per day: | 4.54376217 |
| mean anomaly at epoch: | 6.5248° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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