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 26069U 26040.82732810 +.00000000 +00000-0 +31652-4 0 00000
2 26069 70.9919 218.4408 0009703 130.5938 229.6030 14.13865962 02
| Epoch (UTC): | 09 February 2026 19:51:21 |
| Eccentricity: | 0.0009703 |
| inclination: | 70.9919° |
| perigee height: | 839 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 218.4408° |
| argument of perigee: | 130.5938° |
| revolutions per day: | 14.13865962 |
| mean anomaly at epoch: | 229.6030° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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