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 67289U 26145.14253468 +.00000000 +00000-0 +48614-3 0 00002
2 67289 97.3941 220.5822 0010744 81.8233 278.4223 15.25349319 09
| Epoch (UTC): | 25 May 2026 03:25:14 |
| Eccentricity: | 0.0010744 |
| inclination: | 97.3941° |
| perigee height: | 482 km |
| apogee height: | 497 km |
| right ascension of ascending node: | 220.5822° |
| argument of perigee: | 81.8233° |
| revolutions per day: | 15.25349319 |
| mean anomaly at epoch: | 278.4223° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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