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 35932U 26145.24846162 +.00000000 +00000-0 +18141-3 0 00004
2 35932 98.4052 52.7364 0005517 290.1938 69.8669 14.62429420 07
| Epoch (UTC): | 25 May 2026 05:57:47 |
| Eccentricity: | 0.0005517 |
| inclination: | 98.4052° |
| perigee height: | 681 km |
| apogee height: | 689 km |
| right ascension of ascending node: | 52.7364° |
| argument of perigee: | 290.1938° |
| revolutions per day: | 14.62429420 |
| mean anomaly at epoch: | 69.8669° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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