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 67112U 26145.19458358 +.00000000 +00000-0 +43025-3 0 00008
2 67112 43.0021 97.1913 0001278 264.9044 95.1662 15.27587522 09
| Epoch (UTC): | 25 May 2026 04:40:12 |
| Eccentricity: | 0.0001278 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 97.1913° |
| argument of perigee: | 264.9044° |
| revolutions per day: | 15.27587522 |
| mean anomaly at epoch: | 95.1662° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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