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 26020.94548552 +.00000000 +00000-0 +55120-3 0 00009
2 13121 81.1874 94.1592 0009456 82.4165 277.8143 15.27585050 09
| Epoch (UTC): | 20 January 2026 22:41:29 |
| Eccentricity: | 0.0009456 |
| inclination: | 81.1874° |
| perigee height: | 477 km |
| apogee height: | 490 km |
| right ascension of ascending node: | 94.1592° |
| argument of perigee: | 82.4165° |
| revolutions per day: | 15.27585050 |
| mean anomaly at epoch: | 277.8143° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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