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 67193U 26145.25287361 +.00000000 +00000-0 +12492-3 0 00002
2 67193 70.0018 341.3922 0002625 266.6429 93.4430 14.98334802 03
| Epoch (UTC): | 25 May 2026 06:04:08 |
| Eccentricity: | 0.0002625 |
| inclination: | 70.0018° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 341.3922° |
| argument of perigee: | 266.6429° |
| revolutions per day: | 14.98334802 |
| mean anomaly at epoch: | 93.4430° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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