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 67007U 26145.41883735 +.00000000 +00000-0 +26197-3 0 00008
2 67007 70.0007 260.8900 0002904 271.3266 88.7560 14.98338588 04
| Epoch (UTC): | 25 May 2026 10:03:07 |
| Eccentricity: | 0.0002904 |
| inclination: | 70.0007° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 260.8900° |
| argument of perigee: | 271.3266° |
| revolutions per day: | 14.98338588 |
| mean anomaly at epoch: | 88.7560° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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