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 25991U 26162.22879557 +.00000000 +00000-0 +87176-4 0 00004
2 25991 98.9962 200.7090 0010368 25.5390 59.0722 14.17562796 04
| Epoch (UTC): | 11 June 2026 05:29:27 |
| Eccentricity: | 0.0010368 |
| inclination: | 98.9962° |
| perigee height: | 826 km |
| apogee height: | 841 km |
| right ascension of ascending node: | 200.7090° |
| argument of perigee: | 25.5390° |
| revolutions per day: | 14.17562796 |
| mean anomaly at epoch: | 59.0722° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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