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 67157U 26145.54712097 +.00000000 +00000-0 +48856-3 0 00006
2 67157 51.9001 80.7480 0000547 79.6587 280.4437 14.79943718 00
| Epoch (UTC): | 25 May 2026 13:07:51 |
| Eccentricity: | 0.0000547 |
| inclination: | 51.9001° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 80.7480° |
| argument of perigee: | 79.6587° |
| revolutions per day: | 14.79943718 |
| mean anomaly at epoch: | 280.4437° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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