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 67103U 26144.98043493 +.00000000 +00000-0 +56903-3 0 00003
2 67103 43.0028 98.1722 0001142 264.3059 95.7662 15.27594734 04
| Epoch (UTC): | 24 May 2026 23:31:49 |
| Eccentricity: | 0.0001142 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 98.1722° |
| argument of perigee: | 264.3059° |
| revolutions per day: | 15.27594734 |
| mean anomaly at epoch: | 95.7662° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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