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 26131.67286450 +.00000000 +00000-0 +11977-3 0 00002
2 00082 38.8523 135.4188 1166042 49.2814 320.3430 12.27901331 03
| Epoch (UTC): | 11 May 2026 16:08:55 |
| Eccentricity: | 0.1166042 |
| inclination: | 38.8523° |
| perigee height: | 633 km |
| apogee height: | 2484 km |
| right ascension of ascending node: | 135.4188° |
| argument of perigee: | 49.2814° |
| revolutions per day: | 12.27901331 |
| mean anomaly at epoch: | 320.3430° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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