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 67024U 26145.57756780 +.00000000 +00000-0 +25071-3 0 00003
2 67024 70.0008 260.6386 0003355 264.8154 95.2622 14.98336931 06
| Epoch (UTC): | 25 May 2026 13:51:41 |
| Eccentricity: | 0.0003355 |
| inclination: | 70.0008° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 260.6386° |
| argument of perigee: | 264.8154° |
| revolutions per day: | 14.98336931 |
| mean anomaly at epoch: | 95.2622° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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