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 67649U 26145.33074243 +.00000000 +00000-0 +45816-3 0 00006
2 67649 97.2847 179.5816 0000666 111.4849 248.6464 15.33452256 04
| Epoch (UTC): | 25 May 2026 07:56:16 |
| Eccentricity: | 0.0000666 |
| inclination: | 97.2847° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 179.5816° |
| argument of perigee: | 111.4849° |
| revolutions per day: | 15.33452256 |
| mean anomaly at epoch: | 248.6464° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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