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 68513U 26145.22969292 +.00000000 +00000-0 +10699-2 0 00002
2 68513 53.1605 132.3199 0002654 97.8618 262.2686 15.34425476 02
| Epoch (UTC): | 25 May 2026 05:30:45 |
| Eccentricity: | 0.0002654 |
| inclination: | 53.1605° |
| perigee height: | 461 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 132.3199° |
| argument of perigee: | 97.8618° |
| revolutions per day: | 15.34425476 |
| mean anomaly at epoch: | 262.2686° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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