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 67689U 26145.72867868 +.00000000 +00000-0 +22231-4 0 00003
2 67689 49.9872 21.0925 0005608 309.2973 50.7471 14.91699477 09
| Epoch (UTC): | 25 May 2026 17:29:17 |
| Eccentricity: | 0.0005608 |
| inclination: | 49.9872° |
| perigee height: | 589 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 21.0925° |
| argument of perigee: | 309.2973° |
| revolutions per day: | 14.91699477 |
| mean anomaly at epoch: | 50.7471° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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