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 56226U 26145.39036887 +.00000000 +00000-0 +71404-3 0 00005
2 56226 97.6003 306.3080 0004176 260.1419 99.9382 15.90103068 02
| Epoch (UTC): | 25 May 2026 09:22:07 |
| Eccentricity: | 0.0004176 |
| inclination: | 97.6003° |
| perigee height: | 299 km |
| apogee height: | 305 km |
| right ascension of ascending node: | 306.3080° |
| argument of perigee: | 260.1419° |
| revolutions per day: | 15.90103068 |
| mean anomaly at epoch: | 99.9382° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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