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 67415U 26145.46034852 +.00000000 +00000-0 +83171-3 0 00009
2 67415 43.0007 164.7617 0001639 263.2761 96.7905 15.27608472 05
| Epoch (UTC): | 25 May 2026 11:02:54 |
| Eccentricity: | 0.0001639 |
| inclination: | 43.0007° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 164.7617° |
| argument of perigee: | 263.2761° |
| revolutions per day: | 15.27608472 |
| mean anomaly at epoch: | 96.7905° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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