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 67256U 26145.15043209 +.00000000 +00000-0 +39403-3 0 00003
2 67256 97.3930 220.1005 0017310 85.5108 274.8106 15.22688352 08
| Epoch (UTC): | 25 May 2026 03:36:37 |
| Eccentricity: | 0.0017310 |
| inclination: | 97.3930° |
| perigee height: | 486 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 220.1005° |
| argument of perigee: | 85.5108° |
| revolutions per day: | 15.22688352 |
| mean anomaly at epoch: | 274.8106° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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