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 67998U 26145.56328888 +.00000000 +00000-0 +72281-3 0 00001
2 67998 43.0023 334.4959 0000487 60.2399 299.8501 15.27594256 08
| Epoch (UTC): | 25 May 2026 13:31:08 |
| Eccentricity: | 0.0000487 |
| inclination: | 43.0023° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 334.4959° |
| argument of perigee: | 60.2399° |
| revolutions per day: | 15.27594256 |
| mean anomaly at epoch: | 299.8501° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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