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 26158.80568985 +.00000000 +00000-0 +21289-3 0 00007
2 13121 81.1870 291.1505 0007514 333.2954 26.7893 15.29406824 00
| Epoch (UTC): | 07 June 2026 19:20:11 |
| Eccentricity: | 0.0007514 |
| inclination: | 81.1870° |
| perigee height: | 472 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 291.1505° |
| argument of perigee: | 333.2954° |
| revolutions per day: | 15.29406824 |
| mean anomaly at epoch: | 26.7893° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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