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 68426U 26144.84955602 +.00000000 +00000-0 +48838-3 0 00009
2 68426 97.4529 103.7138 0004005 78.9083 281.2601 15.19155838 07
| Epoch (UTC): | 24 May 2026 20:23:21 |
| Eccentricity: | 0.0004005 |
| inclination: | 97.4529° |
| perigee height: | 506 km |
| apogee height: | 511 km |
| right ascension of ascending node: | 103.7138° |
| argument of perigee: | 78.9083° |
| revolutions per day: | 15.19155838 |
| mean anomaly at epoch: | 281.2601° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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