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 20437U 26108.09269169 +.00000000 +00000-0 +34924-4 0 00004
2 20437 98.8092 156.3388 0011498 81.7858 307.6540 14.33252096 08
| Epoch (UTC): | 18 April 2026 02:13:28 |
| Eccentricity: | 0.0011498 |
| inclination: | 98.8092° |
| perigee height: | 773 km |
| apogee height: | 789 km |
| right ascension of ascending node: | 156.3388° |
| argument of perigee: | 81.7858° |
| revolutions per day: | 14.33252096 |
| mean anomaly at epoch: | 307.6540° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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