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 68740U 26145.58335647 +.00000000 +00000-0 -32385-1 0 00000
2 68740 97.2851 9.2259 0001763 106.2714 201.9917 15.52941545 04
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001763 |
| inclination: | 97.2851° |
| perigee height: | 407 km |
| apogee height: | 409 km |
| right ascension of ascending node: | 9.2259° |
| argument of perigee: | 106.2714° |
| revolutions per day: | 15.52941545 |
| mean anomaly at epoch: | 201.9917° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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