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 65876U 26144.78783519 +.00000000 +00000-0 +42121-3 0 00003
2 65876 53.1602 300.9139 0001209 93.3773 266.7366 15.30208706 08
| Epoch (UTC): | 24 May 2026 18:54:28 |
| Eccentricity: | 0.0001209 |
| inclination: | 53.1602° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 300.9139° |
| argument of perigee: | 93.3773° |
| revolutions per day: | 15.30208706 |
| mean anomaly at epoch: | 266.7366° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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