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 59772U 26145.66317465 +.00000000 +00000-0 -17305-5 0 00001
2 59772 53.1603 29.0542 0001352 76.6778 283.4374 15.31696872 03
| Epoch (UTC): | 25 May 2026 15:54:58 |
| Eccentricity: | 0.0001352 |
| inclination: | 53.1603° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 29.0542° |
| argument of perigee: | 76.6778° |
| revolutions per day: | 15.31696872 |
| mean anomaly at epoch: | 283.4374° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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