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 67856U 26145.45908980 +.00000000 +00000-0 +41270-3 0 00003
2 67856 53.1573 207.3745 0001091 86.1471 273.9655 15.30203904 08
| Epoch (UTC): | 25 May 2026 11:01:05 |
| Eccentricity: | 0.0001091 |
| inclination: | 53.1573° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 207.3745° |
| argument of perigee: | 86.1471° |
| revolutions per day: | 15.30203904 |
| mean anomaly at epoch: | 273.9655° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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