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 44065U 26145.33312814 +.00000000 +00000-0 +00000-0 0 00005
2 44065 6.5052 71.1054 0002318 132.2459 78.9026 0.99335701 06
| Epoch (UTC): | 25 May 2026 07:59:42 |
| Eccentricity: | 0.0002318 |
| inclination: | 6.5052° |
| perigee height: | 36041 km |
| apogee height: | 36061 km |
| right ascension of ascending node: | 71.1054° |
| argument of perigee: | 132.2459° |
| revolutions per day: | 0.99335701 |
| mean anomaly at epoch: | 78.9026° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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