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 67598U 26145.42344993 +.00000000 +00000-0 +73398-3 0 00007
2 67598 97.2861 210.5437 0000357 114.7037 245.4243 15.33455085 03
| Epoch (UTC): | 25 May 2026 10:09:46 |
| Eccentricity: | 0.0000357 |
| inclination: | 97.2861° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 210.5437° |
| argument of perigee: | 114.7037° |
| revolutions per day: | 15.33455085 |
| mean anomaly at epoch: | 245.4243° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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