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 67177U 26145.31788321 +.00000000 +00000-0 +53521-3 0 00001
2 67177 42.9995 238.0220 0001596 246.2695 113.7989 15.27591978 02
| Epoch (UTC): | 25 May 2026 07:37:45 |
| Eccentricity: | 0.0001596 |
| inclination: | 42.9995° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 238.0220° |
| argument of perigee: | 246.2695° |
| revolutions per day: | 15.27591978 |
| mean anomaly at epoch: | 113.7989° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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