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 67798U 26145.45837483 +.00000000 +00000-0 +82190-3 0 00003
2 67798 97.2856 333.5141 0002198 83.2837 276.8656 15.33453438 06
| Epoch (UTC): | 25 May 2026 11:00:03 |
| Eccentricity: | 0.0002198 |
| inclination: | 97.2856° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 333.5141° |
| argument of perigee: | 83.2837° |
| revolutions per day: | 15.33453438 |
| mean anomaly at epoch: | 276.8656° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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