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 67889U 26145.33057588 +.00000000 +00000-0 +55827-3 0 00008
2 67889 97.2855 78.8565 0003104 69.2257 290.9318 15.33446192 04
| Epoch (UTC): | 25 May 2026 07:56:01 |
| Eccentricity: | 0.0003104 |
| inclination: | 97.2855° |
| perigee height: | 463 km |
| apogee height: | 468 km |
| right ascension of ascending node: | 78.8565° |
| argument of perigee: | 69.2257° |
| revolutions per day: | 15.33446192 |
| mean anomaly at epoch: | 290.9318° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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