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 26609U 26038.06163197 +.00000000 +00000-0 +00000-0 0 00008
2 26609 9.6201 10.9292 7946165 137.5655 323.4798 1.25587699 04
| Epoch (UTC): | 07 February 2026 01:28:45 |
| Eccentricity: | 0.7946165 |
| inclination: | 9.6201° |
| perigee height: | 1075 km |
| apogee height: | 58746 km |
| right ascension of ascending node: | 10.9292° |
| argument of perigee: | 137.5655° |
| revolutions per day: | 1.25587699 |
| mean anomaly at epoch: | 323.4798° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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