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 00876U 26073.62406303 +.00000000 +00000-0 +60559-4 0 00005
2 00876 65.0580 245.1523 0150286 296.2674 62.3050 14.65678732 02
| Epoch (UTC): | 14 March 2026 14:58:39 |
| Eccentricity: | 0.0150286 |
| inclination: | 65.0580° |
| perigee height: | 569 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 245.1523° |
| argument of perigee: | 296.2674° |
| revolutions per day: | 14.65678732 |
| mean anomaly at epoch: | 62.3050° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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