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 67575U 26145.41276133 +.00000000 +00000-0 +54556-3 0 00006
2 67575 97.2852 205.7631 0000528 111.4942 248.6357 15.33440640 01
| Epoch (UTC): | 25 May 2026 09:54:22 |
| Eccentricity: | 0.0000528 |
| inclination: | 97.2852° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 205.7631° |
| argument of perigee: | 111.4942° |
| revolutions per day: | 15.33440640 |
| mean anomaly at epoch: | 248.6357° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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