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 68842U 26145.58335647 +.00000000 +00000-0 -32703-1 0 00007
2 68842 97.2845 160.3001 0001885 113.1922 160.4059 15.49625664 00
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001885 |
| inclination: | 97.2845° |
| perigee height: | 417 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 160.3001° |
| argument of perigee: | 113.1922° |
| revolutions per day: | 15.49625664 |
| mean anomaly at epoch: | 160.4059° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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