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 68452U 26145.61814620 +.00000000 +00000-0 +34722-3 0 00005
2 68452 97.4532 104.3747 0005452 125.7817 234.3924 15.17783684 07
| Epoch (UTC): | 25 May 2026 14:50:07 |
| Eccentricity: | 0.0005452 |
| inclination: | 97.4532° |
| perigee height: | 509 km |
| apogee height: | 516 km |
| right ascension of ascending node: | 104.3747° |
| argument of perigee: | 125.7817° |
| revolutions per day: | 15.17783684 |
| mean anomaly at epoch: | 234.3924° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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