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 00876U 26162.59783633 +.00000000 +00000-0 +30412-4 0 00009
2 00876 65.0606 342.2262 0151892 265.1768 93.1977 14.65732681 07
| Epoch (UTC): | 11 June 2026 14:20:53 |
| Eccentricity: | 0.0151892 |
| inclination: | 65.0606° |
| perigee height: | 568 km |
| apogee height: | 782 km |
| right ascension of ascending node: | 342.2262° |
| argument of perigee: | 265.1768° |
| revolutions per day: | 14.65732681 |
| mean anomaly at epoch: | 93.1977° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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