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 26128.11754477 +.00000000 +00000-0 +14805-3 0 00007
2 13121 81.1868 327.4775 0009106 74.4584 285.7656 15.29088657 05
| Epoch (UTC): | 08 May 2026 02:49:15 |
| Eccentricity: | 0.0009106 |
| inclination: | 81.1868° |
| perigee height: | 472 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 327.4775° |
| argument of perigee: | 74.4584° |
| revolutions per day: | 15.29088657 |
| mean anomaly at epoch: | 285.7656° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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