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 67500U 26145.59820953 +.00000000 +00000-0 +56363-3 0 00006
2 67500 43.0028 240.1005 0001418 274.8257 85.2433 15.27594204 02
| Epoch (UTC): | 25 May 2026 14:21:25 |
| Eccentricity: | 0.0001418 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 240.1005° |
| argument of perigee: | 274.8257° |
| revolutions per day: | 15.27594204 |
| mean anomaly at epoch: | 85.2433° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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