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 68119U 26145.41135353 +.00000000 +00000-0 +76033-3 0 00003
2 68119 97.2838 106.0802 0002939 100.7566 259.4008 15.33444455 05
| Epoch (UTC): | 25 May 2026 09:52:20 |
| Eccentricity: | 0.0002939 |
| inclination: | 97.2838° |
| perigee height: | 464 km |
| apogee height: | 468 km |
| right ascension of ascending node: | 106.0802° |
| argument of perigee: | 100.7566° |
| revolutions per day: | 15.33444455 |
| mean anomaly at epoch: | 259.4008° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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