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 15100U 26159.22182190 +.00000000 +00000-0 +11312-4 0 00000
2 15100 82.5312 52.1649 0012669 139.6566 220.5537 13.84556815 07
| Epoch (UTC): | 08 June 2026 05:19:25 |
| Eccentricity: | 0.0012669 |
| inclination: | 82.5312° |
| perigee height: | 938 km |
| apogee height: | 957 km |
| right ascension of ascending node: | 52.1649° |
| argument of perigee: | 139.6566° |
| revolutions per day: | 13.84556815 |
| mean anomaly at epoch: | 220.5537° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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