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 67040U 26145.49808020 +.00000000 +00000-0 +58124-3 0 00002
2 67040 43.0000 324.5189 0001235 294.8048 65.2675 15.27602443 09
| Epoch (UTC): | 25 May 2026 11:57:14 |
| Eccentricity: | 0.0001235 |
| inclination: | 43.0000° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 324.5189° |
| argument of perigee: | 294.8048° |
| revolutions per day: | 15.27602443 |
| mean anomaly at epoch: | 65.2675° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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