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 26129.72009713 +.00000000 +00000-0 +11195-3 0 00002
2 00082 38.8522 142.6735 1166041 39.8211 328.2437 12.27900681 06
| Epoch (UTC): | 09 May 2026 17:16:56 |
| Eccentricity: | 0.1166041 |
| inclination: | 38.8522° |
| perigee height: | 633 km |
| apogee height: | 2484 km |
| right ascension of ascending node: | 142.6735° |
| argument of perigee: | 39.8211° |
| revolutions per day: | 12.27900681 |
| mean anomaly at epoch: | 328.2437° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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