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 67063U 26145.34378450 +.00000000 +00000-0 +91687-4 0 00002
2 67063 50.0026 107.4205 0000831 353.9846 6.1016 13.29328261 07
| Epoch (UTC): | 25 May 2026 08:15:02 |
| Eccentricity: | 0.0000831 |
| inclination: | 50.0026° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 107.4205° |
| argument of perigee: | 353.9846° |
| revolutions per day: | 13.29328261 |
| mean anomaly at epoch: | 6.1016° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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