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 67210U 26145.25704833 +.00000000 +00000-0 +85233-4 0 00004
2 67210 70.0019 341.4052 0002049 270.2283 89.8641 14.98334960 06
| Epoch (UTC): | 25 May 2026 06:10:08 |
| Eccentricity: | 0.0002049 |
| inclination: | 70.0019° |
| perigee height: | 571 km |
| apogee height: | 573 km |
| right ascension of ascending node: | 341.4052° |
| argument of perigee: | 270.2283° |
| revolutions per day: | 14.98334960 |
| mean anomaly at epoch: | 89.8641° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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