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 68525U 26145.25494194 +.00000000 +00000-0 +74630-3 0 00008
2 68525 53.1587 132.4784 0001642 77.8420 282.2767 15.34404928 01
| Epoch (UTC): | 25 May 2026 06:07:06 |
| Eccentricity: | 0.0001642 |
| inclination: | 53.1587° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 132.4784° |
| argument of perigee: | 77.8420° |
| revolutions per day: | 15.34404928 |
| mean anomaly at epoch: | 282.2767° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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