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 26037.92661162 +.00000000 +00000-0 -16172-4 0 00009
2 26069 70.9918 224.5232 0009716 135.9431 224.2467 14.13865938 03
| Epoch (UTC): | 06 February 2026 22:14:19 |
| Eccentricity: | 0.0009716 |
| inclination: | 70.9918° |
| perigee height: | 839 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 224.5232° |
| argument of perigee: | 135.9431° |
| revolutions per day: | 14.13865938 |
| mean anomaly at epoch: | 224.2467° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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