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 44307U 26145.59343514 +.00000000 +00000-0 +00000-0 0 00003
2 44307 0.0182 41.9511 0002672 15.9922 87.8713 1.00271560 03
| Epoch (UTC): | 25 May 2026 14:14:32 |
| Eccentricity: | 0.0002672 |
| inclination: | 0.0182° |
| perigee height: | 35775 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 41.9511° |
| argument of perigee: | 15.9922° |
| revolutions per day: | 1.00271560 |
| mean anomaly at epoch: | 87.8713° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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