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 67244U 26145.57443588 +.00000000 +00000-0 +84898-4 0 00009
2 67244 50.0075 196.7977 0000929 247.5464 112.5310 13.29323481 09
| Epoch (UTC): | 25 May 2026 13:47:11 |
| Eccentricity: | 0.0000929 |
| inclination: | 50.0075° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 196.7977° |
| argument of perigee: | 247.5464° |
| revolutions per day: | 13.29323481 |
| mean anomaly at epoch: | 112.5310° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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