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 67222U 26145.56066406 +.00000000 +00000-0 +16068-3 0 00007
2 67222 45.0022 203.3040 0004326 24.5488 335.5593 15.09182288 09
| Epoch (UTC): | 25 May 2026 13:27:21 |
| Eccentricity: | 0.0004326 |
| inclination: | 45.0022° |
| perigee height: | 536 km |
| apogee height: | 542 km |
| right ascension of ascending node: | 203.3040° |
| argument of perigee: | 24.5488° |
| revolutions per day: | 15.09182288 |
| mean anomaly at epoch: | 335.5593° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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