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 67860U 26145.38227957 +.00000000 +00000-0 +40070-3 0 00005
2 67860 53.1583 208.3023 0000843 83.9704 276.1393 15.30197725 09
| Epoch (UTC): | 25 May 2026 09:10:28 |
| Eccentricity: | 0.0000843 |
| inclination: | 53.1583° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 208.3023° |
| argument of perigee: | 83.9704° |
| revolutions per day: | 15.30197725 |
| mean anomaly at epoch: | 276.1393° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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