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 13403U 26020.94779858 +.00000000 +00000-0 +45798-3 0 00007
2 13403 81.1446 249.4289 0024924 330.0738 29.9068 15.24108913 08
| Epoch (UTC): | 20 January 2026 22:44:49 |
| Eccentricity: | 0.0024924 |
| inclination: | 81.1446° |
| perigee height: | 476 km |
| apogee height: | 511 km |
| right ascension of ascending node: | 249.4289° |
| argument of perigee: | 330.0738° |
| revolutions per day: | 15.24108913 |
| mean anomaly at epoch: | 29.9068° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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