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 67121U 26144.98814514 +.00000000 +00000-0 +62054-3 0 00007
2 67121 43.0044 98.2198 0001084 261.4637 98.6092 15.27589003 07
| Epoch (UTC): | 24 May 2026 23:42:55 |
| Eccentricity: | 0.0001084 |
| inclination: | 43.0044° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 98.2198° |
| argument of perigee: | 261.4637° |
| revolutions per day: | 15.27589003 |
| mean anomaly at epoch: | 98.6092° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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