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 54187U 26145.35222801 +.00000000 +00000-0 +81645-3 0 00006
2 54187 53.2138 19.7922 0001208 114.3001 245.8117 15.08659306 01
| Epoch (UTC): | 25 May 2026 08:27:12 |
| Eccentricity: | 0.0001208 |
| inclination: | 53.2138° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 19.7922° |
| argument of perigee: | 114.3001° |
| revolutions per day: | 15.08659306 |
| mean anomaly at epoch: | 245.8117° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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