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 23604U 26042.17560697 +.00000000 +00000-0 +67351-4 0 00009
2 23604 82.9075 324.8133 0025546 78.7702 281.6323 13.74530529 09
| Epoch (UTC): | 11 February 2026 04:12:52 |
| Eccentricity: | 0.0025546 |
| inclination: | 82.9075° |
| perigee height: | 965 km |
| apogee height: | 1002 km |
| right ascension of ascending node: | 324.8133° |
| argument of perigee: | 78.7702° |
| revolutions per day: | 13.74530529 |
| mean anomaly at epoch: | 281.6323° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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