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 62924U 26145.46233330 +.00000000 +00000-0 +31527-3 0 00009
2 62924 42.9980 55.2947 0000078 32.7311 327.3545 15.27586816 09
| Epoch (UTC): | 25 May 2026 11:05:45 |
| Eccentricity: | 0.0000078 |
| inclination: | 42.9980° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 55.2947° |
| argument of perigee: | 32.7311° |
| revolutions per day: | 15.27586816 |
| mean anomaly at epoch: | 327.3545° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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