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 65177U 26145.22887834 +.00000000 +00000-0 +20663-3 0 00009
2 65177 97.4485 17.6612 0002623 86.6743 273.4784 15.05655806 01
| Epoch (UTC): | 25 May 2026 05:29:35 |
| Eccentricity: | 0.0002623 |
| inclination: | 97.4485° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 17.6612° |
| argument of perigee: | 86.6743° |
| revolutions per day: | 15.05655806 |
| mean anomaly at epoch: | 273.4784° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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