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 67310U 26067.43059698 +.00000000 +00000-0 +15935-2 0 00000
2 67310 42.9944 332.6150 0002033 54.2212 305.8829 15.27597687 07
| Epoch (UTC): | 08 March 2026 10:20:03 |
| Eccentricity: | 0.0002033 |
| inclination: | 42.9944° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 332.6150° |
| argument of perigee: | 54.2212° |
| revolutions per day: | 15.27597687 |
| mean anomaly at epoch: | 305.8829° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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