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 60910U 26145.28629661 +.00000000 +00000-0 +97641-5 0 00009
2 60910 53.1597 113.7534 0001101 89.4095 270.7049 15.69707473 08
| Epoch (UTC): | 25 May 2026 06:52:16 |
| Eccentricity: | 0.0001101 |
| inclination: | 53.1597° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 113.7534° |
| argument of perigee: | 89.4095° |
| revolutions per day: | 15.69707473 |
| mean anomaly at epoch: | 270.7049° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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