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 65129U 26145.61662769 +.00000000 +00000-0 +20062-3 0 00000
2 65129 49.9847 278.4324 0006804 3.5046 356.5939 14.83900307 07
| Epoch (UTC): | 25 May 2026 14:47:56 |
| Eccentricity: | 0.0006804 |
| inclination: | 49.9847° |
| perigee height: | 612 km |
| apogee height: | 622 km |
| right ascension of ascending node: | 278.4324° |
| argument of perigee: | 3.5046° |
| revolutions per day: | 14.83900307 |
| mean anomaly at epoch: | 356.5939° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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