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 67634U 26145.16104051 +.00000000 +00000-0 +90698-3 0 00000
2 67634 43.0033 68.3646 0001212 270.3684 89.7029 15.27592013 00
| Epoch (UTC): | 25 May 2026 03:51:53 |
| Eccentricity: | 0.0001212 |
| inclination: | 43.0033° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 68.3646° |
| argument of perigee: | 270.3684° |
| revolutions per day: | 15.27592013 |
| mean anomaly at epoch: | 89.7029° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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