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 61556U 26145.60209054 +.00000000 +00000-0 +22389-3 0 00007
2 61556 88.9843 58.8843 0008798 133.3207 226.8716 14.16482555 05
| Epoch (UTC): | 25 May 2026 14:27:00 |
| Eccentricity: | 0.0008798 |
| inclination: | 88.9843° |
| perigee height: | 831 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 58.8843° |
| argument of perigee: | 133.3207° |
| revolutions per day: | 14.16482555 |
| mean anomaly at epoch: | 226.8716° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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