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 68124U 26145.58335647 +.00000000 +00000-0 -87661-3 0 00005
2 68124 97.2837 109.1868 0001988 72.3770 249.0492 15.33391558 07
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001988 |
| inclination: | 97.2837° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 109.1868° |
| argument of perigee: | 72.3770° |
| revolutions per day: | 15.33391558 |
| mean anomaly at epoch: | 249.0492° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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