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 53292U 26145.43864939 +.00000000 +00000-0 -86512-4 0 00005
2 53292 53.2111 199.7648 0001466 83.7935 276.3224 15.08843301 01
| Epoch (UTC): | 25 May 2026 10:31:39 |
| Eccentricity: | 0.0001466 |
| inclination: | 53.2111° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 199.7648° |
| argument of perigee: | 83.7935° |
| revolutions per day: | 15.08843301 |
| mean anomaly at epoch: | 276.3224° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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