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 68582U 26145.38418031 +.00000000 +00000-0 +87230-3 0 00001
2 68582 51.8773 287.1057 0002222 272.6743 87.3990 15.36835682 04
| Epoch (UTC): | 25 May 2026 09:13:13 |
| Eccentricity: | 0.0002222 |
| inclination: | 51.8773° |
| perigee height: | 454 km |
| apogee height: | 457 km |
| right ascension of ascending node: | 287.1057° |
| argument of perigee: | 272.6743° |
| revolutions per day: | 15.36835682 |
| mean anomaly at epoch: | 87.3990° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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