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 56722U 26145.48733500 +.00000000 +00000-0 -95850-4 0 00005
2 56722 87.9117 233.2620 0002272 110.9418 249.1957 13.16594266 02
| Epoch (UTC): | 25 May 2026 11:41:45 |
| Eccentricity: | 0.0002272 |
| inclination: | 87.9117° |
| perigee height: | 1196 km |
| apogee height: | 1199 km |
| right ascension of ascending node: | 233.2620° |
| argument of perigee: | 110.9418° |
| revolutions per day: | 13.16594266 |
| mean anomaly at epoch: | 249.1957° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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