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 55173U 26145.34700089 +.00000000 +00000-0 +72002-3 0 00007
2 55173 87.9153 10.4083 0002036 88.2961 271.8404 13.17648077 07
| Epoch (UTC): | 25 May 2026 08:19:40 |
| Eccentricity: | 0.0002036 |
| inclination: | 87.9153° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.4083° |
| argument of perigee: | 88.2961° |
| revolutions per day: | 13.17648077 |
| mean anomaly at epoch: | 271.8404° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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