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 67501U 26145.59435669 +.00000000 +00000-0 +54636-3 0 00004
2 67501 43.0017 240.0667 0001668 262.4365 97.6298 15.27593602 01
| Epoch (UTC): | 25 May 2026 14:15:52 |
| Eccentricity: | 0.0001668 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 240.0667° |
| argument of perigee: | 262.4365° |
| revolutions per day: | 15.27593602 |
| mean anomaly at epoch: | 97.6298° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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