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 67630U 26145.19173031 +.00000000 +00000-0 +89502-3 0 00005
2 67630 43.0031 67.7341 0001715 276.7504 83.3153 15.27609668 01
| Epoch (UTC): | 25 May 2026 04:36:05 |
| Eccentricity: | 0.0001715 |
| inclination: | 43.0031° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 67.7341° |
| argument of perigee: | 276.7504° |
| revolutions per day: | 15.27609668 |
| mean anomaly at epoch: | 83.3153° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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