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 26161.55352963 +.00000000 +00000-0 +19167-3 0 00002
2 13121 81.1868 287.8971 0007397 323.0910 36.9816 15.29435688 02
| Epoch (UTC): | 10 June 2026 13:17:04 |
| Eccentricity: | 0.0007397 |
| inclination: | 81.1868° |
| perigee height: | 472 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 287.8971° |
| argument of perigee: | 323.0910° |
| revolutions per day: | 15.29435688 |
| mean anomaly at epoch: | 36.9816° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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