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 54687U 26145.65222071 +.00000000 +00000-0 +60407-3 0 00006
2 54687 97.6152 330.9325 0002655 156.5312 203.6079 15.83866005 07
| Epoch (UTC): | 25 May 2026 15:39:11 |
| Eccentricity: | 0.0002655 |
| inclination: | 97.6152° |
| perigee height: | 318 km |
| apogee height: | 321 km |
| right ascension of ascending node: | 330.9325° |
| argument of perigee: | 156.5312° |
| revolutions per day: | 15.83866005 |
| mean anomaly at epoch: | 203.6079° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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