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 56156U 26145.42357264 +.00000000 +00000-0 +10383-3 0 00005
2 56156 97.5020 332.8975 0001611 101.3802 258.7610 15.14304527 00
| Epoch (UTC): | 25 May 2026 10:09:56 |
| Eccentricity: | 0.0001611 |
| inclination: | 97.5020° |
| perigee height: | 522 km |
| apogee height: | 524 km |
| right ascension of ascending node: | 332.8975° |
| argument of perigee: | 101.3802° |
| revolutions per day: | 15.14304527 |
| mean anomaly at epoch: | 258.7610° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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