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 67907U 26145.54916351 +.00000000 +00000-0 +52741-3 0 00006
2 67907 42.9998 171.4793 0001685 274.3617 85.7043 15.27589406 08
| Epoch (UTC): | 25 May 2026 13:10:47 |
| Eccentricity: | 0.0001685 |
| inclination: | 42.9998° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 171.4793° |
| argument of perigee: | 274.3617° |
| revolutions per day: | 15.27589406 |
| mean anomaly at epoch: | 85.7043° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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