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 67675U 26145.41625833 +.00000000 +00000-0 +43606-3 0 00006
2 67675 96.6262 209.5134 0016598 214.5478 145.4684 15.24617010 07
| Epoch (UTC): | 25 May 2026 09:59:24 |
| Eccentricity: | 0.0016598 |
| inclination: | 96.6262° |
| perigee height: | 481 km |
| apogee height: | 503 km |
| right ascension of ascending node: | 209.5134° |
| argument of perigee: | 214.5478° |
| revolutions per day: | 15.24617010 |
| mean anomaly at epoch: | 145.4684° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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