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 68536U 26145.25741586 +.00000000 +00000-0 +86117-3 0 00003
2 68536 53.1576 133.2169 0000929 88.5731 271.5382 15.42153238 06
| Epoch (UTC): | 25 May 2026 06:10:40 |
| Eccentricity: | 0.0000929 |
| inclination: | 53.1576° |
| perigee height: | 439 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 133.2169° |
| argument of perigee: | 88.5731° |
| revolutions per day: | 15.42153238 |
| mean anomaly at epoch: | 271.5382° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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