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 08709U 26106.22343939 +.00000000 +00000-0 +27134-4 0 00008
2 08709 69.6729 265.3086 0010570 351.2675 182.3631 13.71740308 05
| Epoch (UTC): | 16 April 2026 05:21:45 |
| Eccentricity: | 0.0010570 |
| inclination: | 69.6729° |
| perigee height: | 986 km |
| apogee height: | 1001 km |
| right ascension of ascending node: | 265.3086° |
| argument of perigee: | 351.2675° |
| revolutions per day: | 13.71740308 |
| mean anomaly at epoch: | 182.3631° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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