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 68762U 26145.74338462 +.00000000 +00000-0 +16356-3 0 00001
2 68762 97.8499 283.4007 0014111 123.6294 236.6281 15.06887043 06
| Epoch (UTC): | 25 May 2026 17:50:28 |
| Eccentricity: | 0.0014111 |
| inclination: | 97.8499° |
| perigee height: | 536 km |
| apogee height: | 555 km |
| right ascension of ascending node: | 283.4007° |
| argument of perigee: | 123.6294° |
| revolutions per day: | 15.06887043 |
| mean anomaly at epoch: | 236.6281° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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