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 44114U 26145.53166036 +.00000000 +00000-0 +00000-0 0 00005
2 44114 0.0330 2.6925 0002600 59.3388 297.9946 5.00115516 00
| Epoch (UTC): | 25 May 2026 12:45:35 |
| Eccentricity: | 0.0002600 |
| inclination: | 0.0330° |
| perigee height: | 8062 km |
| apogee height: | 8070 km |
| right ascension of ascending node: | 2.6925° |
| argument of perigee: | 59.3388° |
| revolutions per day: | 5.00115516 |
| mean anomaly at epoch: | 297.9946° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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