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 67771U 26145.46420282 +.00000000 +00000-0 +51582-3 0 00001
2 67771 51.8801 209.4123 0011291 338.6613 21.3901 15.35371551 00
| Epoch (UTC): | 25 May 2026 11:08:27 |
| Eccentricity: | 0.0011291 |
| inclination: | 51.8801° |
| perigee height: | 452 km |
| apogee height: | 468 km |
| right ascension of ascending node: | 209.4123° |
| argument of perigee: | 338.6613° |
| revolutions per day: | 15.35371551 |
| mean anomaly at epoch: | 21.3901° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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