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 60915U 26145.19810714 +.00000000 +00000-0 +41544-5 0 00006
2 60915 53.1586 113.9013 0001046 69.2921 290.8209 15.69698594 01
| Epoch (UTC): | 25 May 2026 04:45:16 |
| Eccentricity: | 0.0001046 |
| inclination: | 53.1586° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 113.9013° |
| argument of perigee: | 69.2921° |
| revolutions per day: | 15.69698594 |
| mean anomaly at epoch: | 290.8209° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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