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 67194U 26145.00672485 +.00000000 +00000-0 +34086-3 0 00004
2 67194 70.0021 342.1424 0002964 261.2348 98.8476 14.98337619 09
| Epoch (UTC): | 25 May 2026 00:09:41 |
| Eccentricity: | 0.0002964 |
| inclination: | 70.0021° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 342.1424° |
| argument of perigee: | 261.2348° |
| revolutions per day: | 14.98337619 |
| mean anomaly at epoch: | 98.8476° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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