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 60992U 26144.82834683 +.00000000 +00000-0 +17047-4 0 00001
2 60992 53.1588 265.8886 0001138 64.6749 295.4387 15.69715709 08
| Epoch (UTC): | 24 May 2026 19:52:49 |
| Eccentricity: | 0.0001138 |
| inclination: | 53.1588° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 265.8886° |
| argument of perigee: | 64.6749° |
| revolutions per day: | 15.69715709 |
| mean anomaly at epoch: | 295.4387° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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