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 11289U 26161.59951175 +.00000000 +00000-0 -72893-5 0 00007
2 11289 81.2456 202.9212 0074076 282.8677 76.4226 14.12111960 04
| Epoch (UTC): | 10 June 2026 14:23:17 |
| Eccentricity: | 0.0074076 |
| inclination: | 81.2456° |
| perigee height: | 799 km |
| apogee height: | 906 km |
| right ascension of ascending node: | 202.9212° |
| argument of perigee: | 282.8677° |
| revolutions per day: | 14.12111960 |
| mean anomaly at epoch: | 76.4226° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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