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 52452U 26145.23022916 +.00000000 +00000-0 -17380-4 0 00008
2 52452 53.2143 85.3877 0001251 71.7385 288.3743 15.08845200 04
| Epoch (UTC): | 25 May 2026 05:31:31 |
| Eccentricity: | 0.0001251 |
| inclination: | 53.2143° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 85.3877° |
| argument of perigee: | 71.7385° |
| revolutions per day: | 15.08845200 |
| mean anomaly at epoch: | 288.3743° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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