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 52184U 26145.59226560 +.00000000 +00000-0 +54747-3 0 00006
2 52184 97.2347 224.8632 0004596 340.1295 19.9772 15.41344381 08
| Epoch (UTC): | 25 May 2026 14:12:51 |
| Eccentricity: | 0.0004596 |
| inclination: | 97.2347° |
| perigee height: | 439 km |
| apogee height: | 445 km |
| right ascension of ascending node: | 224.8632° |
| argument of perigee: | 340.1295° |
| revolutions per day: | 15.41344381 |
| mean anomaly at epoch: | 19.9772° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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