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 67633U 26145.05967574 +.00000000 +00000-0 +55642-3 0 00004
2 67633 43.0015 68.4611 0000998 283.6162 76.4579 15.27596022 07
| Epoch (UTC): | 25 May 2026 01:25:55 |
| Eccentricity: | 0.0000998 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 68.4611° |
| argument of perigee: | 283.6162° |
| revolutions per day: | 15.27596022 |
| mean anomaly at epoch: | 76.4579° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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