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 67925U 26131.60514954 +.00000000 +00000-0 +55244-3 0 00002
2 67925 43.0008 250.0044 0001510 282.1418 77.9265 15.27590205 06
| Epoch (UTC): | 11 May 2026 14:31:24 |
| Eccentricity: | 0.0001510 |
| inclination: | 43.0008° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 250.0044° |
| argument of perigee: | 282.1418° |
| revolutions per day: | 15.27590205 |
| mean anomaly at epoch: | 77.9265° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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