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 67515U 26145.59563953 +.00000000 +00000-0 +88810-3 0 00008
2 67515 43.0029 240.0789 0001711 271.9665 88.0991 15.27602390 00
| Epoch (UTC): | 25 May 2026 14:17:43 |
| Eccentricity: | 0.0001711 |
| inclination: | 43.0029° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 240.0789° |
| argument of perigee: | 271.9665° |
| revolutions per day: | 15.27602390 |
| mean anomaly at epoch: | 88.0991° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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