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 55150U 26145.51052137 +.00000000 +00000-0 +15234-3 0 00009
2 55150 87.9159 339.9827 0001013 128.7948 231.3275 13.18687215 07
| Epoch (UTC): | 25 May 2026 12:15:09 |
| Eccentricity: | 0.0001013 |
| inclination: | 87.9159° |
| perigee height: | 1189 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 339.9827° |
| argument of perigee: | 128.7948° |
| revolutions per day: | 13.18687215 |
| mean anomaly at epoch: | 231.3275° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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