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 68534U 26145.26125001 +.00000000 +00000-0 +64024-3 0 00003
2 68534 53.1585 132.5162 0001176 90.6050 269.5088 15.34414067 03
| Epoch (UTC): | 25 May 2026 06:16:12 |
| Eccentricity: | 0.0001176 |
| inclination: | 53.1585° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 132.5162° |
| argument of perigee: | 90.6050° |
| revolutions per day: | 15.34414067 |
| mean anomaly at epoch: | 269.5088° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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