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 67898U 26145.32784432 +.00000000 +00000-0 +19489-3 0 00006
2 67898 97.2844 78.8615 0001876 89.3879 270.7578 15.33442251 01
| Epoch (UTC): | 25 May 2026 07:52:05 |
| Eccentricity: | 0.0001876 |
| inclination: | 97.2844° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 78.8615° |
| argument of perigee: | 89.3879° |
| revolutions per day: | 15.33442251 |
| mean anomaly at epoch: | 270.7578° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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