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 13778U 26072.85144106 +.00000000 +00000-0 +40491-4 0 00007
2 13778 100.0760 114.2363 0021027 177.3766 182.7514 14.09694096 07
| Epoch (UTC): | 13 March 2026 20:26:04 |
| Eccentricity: | 0.0021027 |
| inclination: | 100.0760° |
| perigee height: | 845 km |
| apogee height: | 876 km |
| right ascension of ascending node: | 114.2363° |
| argument of perigee: | 177.3766° |
| revolutions per day: | 14.09694096 |
| mean anomaly at epoch: | 182.7514° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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