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 11574U 26072.42155192 +.00000000 +00000-0 +10293-3 0 00005
2 11574 74.0667 84.1345 0017114 256.4414 103.4836 14.42353288 00
| Epoch (UTC): | 13 March 2026 10:07:02 |
| Eccentricity: | 0.0017114 |
| inclination: | 74.0667° |
| perigee height: | 739 km |
| apogee height: | 763 km |
| right ascension of ascending node: | 84.1345° |
| argument of perigee: | 256.4414° |
| revolutions per day: | 14.42353288 |
| mean anomaly at epoch: | 103.4836° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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