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 68519U 26145.24862675 +.00000000 +00000-0 +79775-3 0 00008
2 68519 53.1586 132.4401 0000483 77.8906 282.2151 15.34405990 07
| Epoch (UTC): | 25 May 2026 05:58:01 |
| Eccentricity: | 0.0000483 |
| inclination: | 53.1586° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 132.4401° |
| argument of perigee: | 77.8906° |
| revolutions per day: | 15.34405990 |
| mean anomaly at epoch: | 282.2151° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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