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 56225U 26145.53714543 +.00000000 +00000-0 +10648-3 0 00005
2 56225 97.3719 22.6895 0009270 193.6892 166.4089 15.12428567 01
| Epoch (UTC): | 25 May 2026 12:53:29 |
| Eccentricity: | 0.0009270 |
| inclination: | 97.3719° |
| perigee height: | 522 km |
| apogee height: | 535 km |
| right ascension of ascending node: | 22.6895° |
| argument of perigee: | 193.6892° |
| revolutions per day: | 15.12428567 |
| mean anomaly at epoch: | 166.4089° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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