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 60320U 26144.86112681 +.00000000 +00000-0 +26050-4 0 00001
2 60320 53.1618 303.1694 0000998 106.7957 253.3153 15.30198396 01
| Epoch (UTC): | 24 May 2026 20:40:01 |
| Eccentricity: | 0.0000998 |
| inclination: | 53.1618° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 303.1694° |
| argument of perigee: | 106.7957° |
| revolutions per day: | 15.30198396 |
| mean anomaly at epoch: | 253.3153° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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