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 60364U 26145.48426616 +.00000000 +00000-0 +49477-4 0 00002
2 60364 53.1614 313.0112 0001168 76.9642 283.1489 15.30199485 02
| Epoch (UTC): | 25 May 2026 11:37:20 |
| Eccentricity: | 0.0001168 |
| inclination: | 53.1614° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 313.0112° |
| argument of perigee: | 76.9642° |
| revolutions per day: | 15.30199485 |
| mean anomaly at epoch: | 283.1489° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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