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 18403U 26087.87159925 +.00000000 +00000-0 +19591-4 0 00007
2 18403 82.9191 222.2731 0056893 215.6202 144.1153 13.76831325 04
| Epoch (UTC): | 28 March 2026 20:55:06 |
| Eccentricity: | 0.0056893 |
| inclination: | 82.9191° |
| perigee height: | 933 km |
| apogee height: | 1017 km |
| right ascension of ascending node: | 222.2731° |
| argument of perigee: | 215.6202° |
| revolutions per day: | 13.76831325 |
| mean anomaly at epoch: | 144.1153° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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