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 26064.15353697 +.00000000 +00000-0 +11176-3 0 00008
2 10521 74.0264 131.9235 0018988 88.5511 271.7820 14.42390603 09
| Epoch (UTC): | 05 March 2026 03:41:05 |
| Eccentricity: | 0.0018988 |
| inclination: | 74.0264° |
| perigee height: | 737 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 131.9235° |
| argument of perigee: | 88.5511° |
| revolutions per day: | 14.42390603 |
| mean anomaly at epoch: | 271.7820° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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