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 51732U 26145.23670259 +.00000000 +00000-0 +57439-3 0 00004
2 51732 53.2130 335.4911 0001602 85.4178 274.6997 15.08794143 08
| Epoch (UTC): | 25 May 2026 05:40:51 |
| Eccentricity: | 0.0001602 |
| inclination: | 53.2130° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 335.4911° |
| argument of perigee: | 85.4178° |
| revolutions per day: | 15.08794143 |
| mean anomaly at epoch: | 274.6997° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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