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 26021.47301426 +.00000000 +00000-0 +35941-3 0 00007
2 13403 81.1444 248.8093 0024899 328.3414 31.6319 15.24121225 04
| Epoch (UTC): | 21 January 2026 11:21:08 |
| Eccentricity: | 0.0024899 |
| inclination: | 81.1444° |
| perigee height: | 476 km |
| apogee height: | 511 km |
| right ascension of ascending node: | 248.8093° |
| argument of perigee: | 328.3414° |
| revolutions per day: | 15.24121225 |
| mean anomaly at epoch: | 31.6319° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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