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 67913U 26145.39270448 +.00000000 +00000-0 +48069-3 0 00004
2 67913 43.0032 172.0068 0001413 269.1887 90.8802 15.27581650 01
| Epoch (UTC): | 25 May 2026 09:25:29 |
| Eccentricity: | 0.0001413 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 172.0068° |
| argument of perigee: | 269.1887° |
| revolutions per day: | 15.27581650 |
| mean anomaly at epoch: | 90.8802° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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