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 68257U 26145.43947830 +.00000000 +00000-0 +82976-3 0 00002
2 68257 53.1594 293.8411 0001120 118.6107 241.5008 15.34414146 06
| Epoch (UTC): | 25 May 2026 10:32:50 |
| Eccentricity: | 0.0001120 |
| inclination: | 53.1594° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 293.8411° |
| argument of perigee: | 118.6107° |
| revolutions per day: | 15.34414146 |
| mean anomaly at epoch: | 241.5008° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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