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 26134.35783610 +.00000000 +00000-0 +13319-3 0 00002
2 00082 38.8525 125.4442 1166040 62.2881 309.1188 12.27902342 02
| Epoch (UTC): | 14 May 2026 08:35:17 |
| Eccentricity: | 0.1166040 |
| inclination: | 38.8525° |
| perigee height: | 633 km |
| apogee height: | 2484 km |
| right ascension of ascending node: | 125.4442° |
| argument of perigee: | 62.2881° |
| revolutions per day: | 12.27902342 |
| mean anomaly at epoch: | 309.1188° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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