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 55147U 26145.29806370 +.00000000 +00000-0 +15181-3 0 00007
2 55147 87.9160 340.0278 0001490 95.3430 264.7873 13.18685815 00
| Epoch (UTC): | 25 May 2026 07:09:12 |
| Eccentricity: | 0.0001490 |
| inclination: | 87.9160° |
| perigee height: | 1189 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 340.0278° |
| argument of perigee: | 95.3430° |
| revolutions per day: | 13.18685815 |
| mean anomaly at epoch: | 264.7873° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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