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 65104U 26145.64965935 +.00000000 +00000-0 +15518-2 0 00006
2 65104 53.1608 26.2807 0002865 76.7315 283.4010 15.42234899 01
| Epoch (UTC): | 25 May 2026 15:35:30 |
| Eccentricity: | 0.0002865 |
| inclination: | 53.1608° |
| perigee height: | 438 km |
| apogee height: | 441 km |
| right ascension of ascending node: | 26.2807° |
| argument of perigee: | 76.7315° |
| revolutions per day: | 15.42234899 |
| mean anomaly at epoch: | 283.4010° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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