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 67549U 26145.24724913 +.00000000 +00000-0 +64514-3 0 00007
2 67549 97.2866 32.2545 0001599 92.1461 267.9965 15.33460583 01
| Epoch (UTC): | 25 May 2026 05:56:02 |
| Eccentricity: | 0.0001599 |
| inclination: | 97.2866° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 32.2545° |
| argument of perigee: | 92.1461° |
| revolutions per day: | 15.33460583 |
| mean anomaly at epoch: | 267.9965° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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