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 68524U 26145.25704543 +.00000000 +00000-0 +95814-3 0 00006
2 68524 53.1581 132.4949 0001495 103.6401 256.4769 15.34408655 06
| Epoch (UTC): | 25 May 2026 06:10:08 |
| Eccentricity: | 0.0001495 |
| inclination: | 53.1581° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 132.4949° |
| argument of perigee: | 103.6401° |
| revolutions per day: | 15.34408655 |
| mean anomaly at epoch: | 256.4769° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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