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 68667U 26145.60466031 +.00000000 +00000-0 +58178-3 0 00002
2 68667 97.2873 17.1484 0002461 99.0744 261.0777 15.33452299 05
| Epoch (UTC): | 25 May 2026 14:30:42 |
| Eccentricity: | 0.0002461 |
| inclination: | 97.2873° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 17.1484° |
| argument of perigee: | 99.0744° |
| revolutions per day: | 15.33452299 |
| mean anomaly at epoch: | 261.0777° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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