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 10121U 26044.57928631 +.00000000 +00000-0 +94442-4 0 00002
2 10121 74.0443 85.9837 0018115 12.0879 348.0705 14.37341311 07
| Epoch (UTC): | 13 February 2026 13:54:10 |
| Eccentricity: | 0.0018115 |
| inclination: | 74.0443° |
| perigee height: | 754 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 85.9837° |
| argument of perigee: | 12.0879° |
| revolutions per day: | 14.37341311 |
| mean anomaly at epoch: | 348.0705° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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