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 26071.07705500 +.00000000 +00000-0 +21101-4 0 00008
2 13778 100.0764 112.2521 0020971 182.1567 177.9512 14.09693674 00
| Epoch (UTC): | 12 March 2026 01:50:57 |
| Eccentricity: | 0.0020971 |
| inclination: | 100.0764° |
| perigee height: | 845 km |
| apogee height: | 876 km |
| right ascension of ascending node: | 112.2521° |
| argument of perigee: | 182.1567° |
| revolutions per day: | 14.09693674 |
| mean anomaly at epoch: | 177.9512° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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