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 68074U 26145.38508005 +.00000000 +00000-0 +37698-3 0 00001
2 68074 53.1591 182.0684 0000919 83.5020 276.6088 15.34399149 02
| Epoch (UTC): | 25 May 2026 09:14:30 |
| Eccentricity: | 0.0000919 |
| inclination: | 53.1591° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 182.0684° |
| argument of perigee: | 83.5020° |
| revolutions per day: | 15.34399149 |
| mean anomaly at epoch: | 276.6088° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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