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 67120U 26145.26382046 +.00000000 +00000-0 +49514-3 0 00004
2 67120 43.0014 96.8503 0002274 253.4867 106.5735 15.27594139 04
| Epoch (UTC): | 25 May 2026 06:19:54 |
| Eccentricity: | 0.0002274 |
| inclination: | 43.0014° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 96.8503° |
| argument of perigee: | 253.4867° |
| revolutions per day: | 15.27594139 |
| mean anomaly at epoch: | 106.5735° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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