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 68555U 26145.31758588 +.00000000 +00000-0 +93274-3 0 00003
2 68555 53.1594 6.1658 0001065 86.8910 273.2215 15.34382157 09
| Epoch (UTC): | 25 May 2026 07:37:19 |
| Eccentricity: | 0.0001065 |
| inclination: | 53.1594° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 6.1658° |
| argument of perigee: | 86.8910° |
| revolutions per day: | 15.34382157 |
| mean anomaly at epoch: | 273.2215° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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