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 26127.85236828 +.00000000 +00000-0 +22331-4 0 00003
2 23604 82.9029 261.0326 0023860 196.7290 163.3082 13.74549102 09
| Epoch (UTC): | 07 May 2026 20:27:24 |
| Eccentricity: | 0.0023860 |
| inclination: | 82.9029° |
| perigee height: | 966 km |
| apogee height: | 1001 km |
| right ascension of ascending node: | 261.0326° |
| argument of perigee: | 196.7290° |
| revolutions per day: | 13.74549102 |
| mean anomaly at epoch: | 163.3082° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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