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 67916U 26145.44393784 +.00000000 +00000-0 +50853-3 0 00006
2 67916 43.0013 171.5287 0001382 266.7518 93.3176 15.27586108 04
| Epoch (UTC): | 25 May 2026 10:39:16 |
| Eccentricity: | 0.0001382 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 171.5287° |
| argument of perigee: | 266.7518° |
| revolutions per day: | 15.27586108 |
| mean anomaly at epoch: | 93.3176° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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