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 26108.84409167 +.00000000 +00000-0 +17877-4 0 00007
2 08709 69.6730 259.8463 0010710 348.2245 163.7539 13.71740370 08
| Epoch (UTC): | 18 April 2026 20:15:29 |
| Eccentricity: | 0.0010710 |
| inclination: | 69.6730° |
| perigee height: | 985 km |
| apogee height: | 1001 km |
| right ascension of ascending node: | 259.8463° |
| argument of perigee: | 348.2245° |
| revolutions per day: | 13.71740370 |
| mean anomaly at epoch: | 163.7539° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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