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 26084.98097569 +.00000000 +00000-0 +00000-0 0 00009
2 26609 9.5470 3.8186 7939703 152.3644 295.7300 1.25588352 04
| Epoch (UTC): | 25 March 2026 23:32:36 |
| Eccentricity: | 0.7939703 |
| inclination: | 9.5470° |
| perigee height: | 1098 km |
| apogee height: | 58722 km |
| right ascension of ascending node: | 3.8186° |
| argument of perigee: | 152.3644° |
| revolutions per day: | 1.25588352 |
| mean anomaly at epoch: | 295.7300° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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