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 68014U 26145.56455750 +.00000000 +00000-0 +11056-2 0 00002
2 68014 43.0024 334.4851 0003233 265.2596 94.7887 15.27627815 05
| Epoch (UTC): | 25 May 2026 13:32:57 |
| Eccentricity: | 0.0003233 |
| inclination: | 43.0024° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 334.4851° |
| argument of perigee: | 265.2596° |
| revolutions per day: | 15.27627815 |
| mean anomaly at epoch: | 94.7887° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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