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 15516U 26087.86722120 +.00000000 +00000-0 +71532-4 0 00004
2 15516 82.5335 35.8978 0016302 141.3688 218.8643 13.85861073 03
| Epoch (UTC): | 28 March 2026 20:48:47 |
| Eccentricity: | 0.0016302 |
| inclination: | 82.5335° |
| perigee height: | 931 km |
| apogee height: | 955 km |
| right ascension of ascending node: | 35.8978° |
| argument of perigee: | 141.3688° |
| revolutions per day: | 13.85861073 |
| mean anomaly at epoch: | 218.8643° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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