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 57184U 26088.18452352 +.00000000 +00000-0 +36717-3 0 00009
2 57184 97.5165 146.9949 0012139 38.3154 321.8940 15.18143174 04
| Epoch (UTC): | 29 March 2026 04:25:42 |
| Eccentricity: | 0.0012139 |
| inclination: | 97.5165° |
| perigee height: | 503 km |
| apogee height: | 520 km |
| right ascension of ascending node: | 146.9949° |
| argument of perigee: | 38.3154° |
| revolutions per day: | 15.18143174 |
| mean anomaly at epoch: | 321.8940° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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