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 13121U 26017.93225429 +.00000000 +00000-0 +21881-3 0 00006
2 13121 81.1884 97.7162 0009449 91.5187 268.7130 15.27521214 06
| Epoch (UTC): | 17 January 2026 22:22:26 |
| Eccentricity: | 0.0009449 |
| inclination: | 81.1884° |
| perigee height: | 477 km |
| apogee height: | 490 km |
| right ascension of ascending node: | 97.7162° |
| argument of perigee: | 91.5187° |
| revolutions per day: | 15.27521214 |
| mean anomaly at epoch: | 268.7130° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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