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 67416U 26145.38980443 +.00000000 +00000-0 +34212-3 0 00009
2 67416 43.0006 165.0944 0001427 272.4592 87.6096 15.27587461 05
| Epoch (UTC): | 25 May 2026 09:21:19 |
| Eccentricity: | 0.0001427 |
| inclination: | 43.0006° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 165.0944° |
| argument of perigee: | 272.4592° |
| revolutions per day: | 15.27587461 |
| mean anomaly at epoch: | 87.6096° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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