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 67648U 26145.33198506 +.00000000 +00000-0 +44734-3 0 00002
2 67648 97.2855 178.5153 0000971 75.2712 284.8638 15.33452737 09
| Epoch (UTC): | 25 May 2026 07:58:03 |
| Eccentricity: | 0.0000971 |
| inclination: | 97.2855° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 178.5153° |
| argument of perigee: | 75.2712° |
| revolutions per day: | 15.33452737 |
| mean anomaly at epoch: | 284.8638° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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