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 67138U 26145.50510510 +.00000000 +00000-0 +43614-3 0 00004
2 67138 51.8948 75.2809 0008948 327.7076 32.3343 14.92577585 05
| Epoch (UTC): | 25 May 2026 12:07:21 |
| Eccentricity: | 0.0008948 |
| inclination: | 51.8948° |
| perigee height: | 584 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 75.2809° |
| argument of perigee: | 327.7076° |
| revolutions per day: | 14.92577585 |
| mean anomaly at epoch: | 32.3343° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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