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 10521U 26074.55711237 +.00000000 +00000-0 +86806-4 0 00004
2 10521 74.0248 112.6141 0019049 65.2450 295.0686 14.42397723 05
| Epoch (UTC): | 15 March 2026 13:22:14 |
| Eccentricity: | 0.0019049 |
| inclination: | 74.0248° |
| perigee height: | 737 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 112.6141° |
| argument of perigee: | 65.2450° |
| revolutions per day: | 14.42397723 |
| mean anomaly at epoch: | 295.0686° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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