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 68346U 26145.58335647 +.00000000 +00000-0 +76110-3 0 00007
2 68346 53.1592 347.2028 0001048 80.7637 259.4416 15.34380720 08
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001048 |
| inclination: | 53.1592° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 347.2028° |
| argument of perigee: | 80.7637° |
| revolutions per day: | 15.34380720 |
| mean anomaly at epoch: | 259.4416° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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