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 15755U 26066.18034611 +.00000000 +00000-0 +11747-4 0 00004
2 15755 71.1113 131.2539 0033809 146.0744 214.2554 14.20990030 03
| Epoch (UTC): | 07 March 2026 04:19:41 |
| Eccentricity: | 0.0033809 |
| inclination: | 71.1113° |
| perigee height: | 798 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 131.2539° |
| argument of perigee: | 146.0744° |
| revolutions per day: | 14.20990030 |
| mean anomaly at epoch: | 214.2554° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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