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 26106.65882920 +.00000000 +00000-0 +13613-3 0 00007
2 35932 98.4071 13.4711 0007875 50.7783 309.4116 14.62359440 09
| Epoch (UTC): | 16 April 2026 15:48:42 |
| Eccentricity: | 0.0007875 |
| inclination: | 98.4071° |
| perigee height: | 680 km |
| apogee height: | 691 km |
| right ascension of ascending node: | 13.4711° |
| argument of perigee: | 50.7783° |
| revolutions per day: | 14.62359440 |
| mean anomaly at epoch: | 309.4116° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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