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 53291U 26145.43352899 +.00000000 +00000-0 +68723-4 0 00004
2 53291 53.2128 194.3935 0001429 87.8636 272.2520 15.08859038 08
| Epoch (UTC): | 25 May 2026 10:24:16 |
| Eccentricity: | 0.0001429 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 194.3935° |
| argument of perigee: | 87.8636° |
| revolutions per day: | 15.08859038 |
| mean anomaly at epoch: | 272.2520° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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