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 26072.86786791 +.00000000 +00000-0 +71765-4 0 00005
2 15755 71.1102 117.1506 0033445 135.1722 225.2116 14.20990837 00
| Epoch (UTC): | 13 March 2026 20:49:43 |
| Eccentricity: | 0.0033445 |
| inclination: | 71.1102° |
| perigee height: | 798 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 117.1506° |
| argument of perigee: | 135.1722° |
| revolutions per day: | 14.20990837 |
| mean anomaly at epoch: | 225.2116° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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