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 56155U 26145.42357519 +.00000000 +00000-0 +10030-3 0 00006
2 56155 97.5030 332.8894 0001755 81.5756 278.5675 15.14303596 02
| Epoch (UTC): | 25 May 2026 10:09:56 |
| Eccentricity: | 0.0001755 |
| inclination: | 97.5030° |
| perigee height: | 522 km |
| apogee height: | 524 km |
| right ascension of ascending node: | 332.8894° |
| argument of perigee: | 81.5756° |
| revolutions per day: | 15.14303596 |
| mean anomaly at epoch: | 278.5675° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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