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 00082U 26041.20596465 +.00000000 +00000-0 +26873-3 0 00002
2 00082 38.8592 111.4486 1167621 331.2878 22.8070 12.27856056 09
| Epoch (UTC): | 10 February 2026 04:56:35 |
| Eccentricity: | 0.1167621 |
| inclination: | 38.8592° |
| perigee height: | 632 km |
| apogee height: | 2485 km |
| right ascension of ascending node: | 111.4486° |
| argument of perigee: | 331.2878° |
| revolutions per day: | 12.27856056 |
| mean anomaly at epoch: | 22.8070° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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