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 26067.13590119 +.00000000 +00000-0 +11682-3 0 00003
2 10521 74.0259 126.3885 0018993 81.9112 278.4197 14.42393096 02
| Epoch (UTC): | 08 March 2026 03:15:41 |
| Eccentricity: | 0.0018993 |
| inclination: | 74.0259° |
| perigee height: | 737 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 126.3885° |
| argument of perigee: | 81.9112° |
| revolutions per day: | 14.42393096 |
| mean anomaly at epoch: | 278.4197° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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