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 68459U 26145.30858700 +.00000000 +00000-0 +28643-3 0 00000
2 68459 97.4514 104.0102 0007426 131.8772 228.3097 15.17165907 03
| Epoch (UTC): | 25 May 2026 07:24:21 |
| Eccentricity: | 0.0007426 |
| inclination: | 97.4514° |
| perigee height: | 509 km |
| apogee height: | 520 km |
| right ascension of ascending node: | 104.0102° |
| argument of perigee: | 131.8772° |
| revolutions per day: | 15.17165907 |
| mean anomaly at epoch: | 228.3097° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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