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 67638U 26145.48411787 +.00000000 +00000-0 +81790-3 0 00009
2 67638 43.0054 66.4772 0000645 262.9962 97.0816 15.27588750 00
| Epoch (UTC): | 25 May 2026 11:37:07 |
| Eccentricity: | 0.0000645 |
| inclination: | 43.0054° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 66.4772° |
| argument of perigee: | 262.9962° |
| revolutions per day: | 15.27588750 |
| mean anomaly at epoch: | 97.0816° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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