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 67885U 26145.53993100 +.00000000 +00000-0 +64237-3 0 00000
2 67885 97.2852 79.0298 0001980 92.9045 267.2424 15.33448070 03
| Epoch (UTC): | 25 May 2026 12:57:30 |
| Eccentricity: | 0.0001980 |
| inclination: | 97.2852° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 79.0298° |
| argument of perigee: | 92.9045° |
| revolutions per day: | 15.33448070 |
| mean anomaly at epoch: | 267.2424° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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