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 26130.53877126 +.00000000 +00000-0 +13674-3 0 00006
2 13121 81.1867 324.6122 0009054 67.1104 293.1086 15.29108077 07
| Epoch (UTC): | 10 May 2026 12:55:49 |
| Eccentricity: | 0.0009054 |
| inclination: | 81.1867° |
| perigee height: | 472 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 324.6122° |
| argument of perigee: | 67.1104° |
| revolutions per day: | 15.29108077 |
| mean anomaly at epoch: | 293.1086° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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