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 44047U 26145.64773964 +.00000000 +00000-0 +86520-4 0 00001
2 44047 98.0045 210.7373 0001173 82.9190 277.2151 14.72276004 09
| Epoch (UTC): | 25 May 2026 15:32:44 |
| Eccentricity: | 0.0001173 |
| inclination: | 98.0045° |
| perigee height: | 653 km |
| apogee height: | 655 km |
| right ascension of ascending node: | 210.7373° |
| argument of perigee: | 82.9190° |
| revolutions per day: | 14.72276004 |
| mean anomaly at epoch: | 277.2151° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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