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 26145.33960640 +.00000000 +00000-0 +00000-0 0 00005
2 26609 9.4601 354.5078 7931330 171.3121 224.1265 1.25588206 08
| Epoch (UTC): | 25 May 2026 08:09:01 |
| Eccentricity: | 0.7931330 |
| inclination: | 9.4601° |
| perigee height: | 1129 km |
| apogee height: | 58692 km |
| right ascension of ascending node: | 354.5078° |
| argument of perigee: | 171.3121° |
| revolutions per day: | 1.25588206 |
| mean anomaly at epoch: | 224.1265° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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