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 65833U 26145.55408667 +.00000000 +00000-0 +78069-3 0 00000
2 65833 53.1584 91.1726 0002004 83.2170 276.9059 15.30202591 02
| Epoch (UTC): | 25 May 2026 13:17:53 |
| Eccentricity: | 0.0002004 |
| inclination: | 53.1584° |
| perigee height: | 474 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 91.1726° |
| argument of perigee: | 83.2170° |
| revolutions per day: | 15.30202591 |
| mean anomaly at epoch: | 276.9059° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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