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 68082U 26145.49010172 +.00000000 +00000-0 +54013-3 0 00005
2 68082 53.1583 181.2721 0001141 64.5588 295.5533 15.34396606 01
| Epoch (UTC): | 25 May 2026 11:45:44 |
| Eccentricity: | 0.0001141 |
| inclination: | 53.1583° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 181.2721° |
| argument of perigee: | 64.5588° |
| revolutions per day: | 15.34396606 |
| mean anomaly at epoch: | 295.5533° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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