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 67220U 26145.52021203 +.00000000 +00000-0 +36909-3 0 00003
2 67220 45.0014 203.8308 0003687 14.6497 345.4485 15.08572249 08
| Epoch (UTC): | 25 May 2026 12:29:06 |
| Eccentricity: | 0.0003687 |
| inclination: | 45.0014° |
| perigee height: | 538 km |
| apogee height: | 543 km |
| right ascension of ascending node: | 203.8308° |
| argument of perigee: | 14.6497° |
| revolutions per day: | 15.08572249 |
| mean anomaly at epoch: | 345.4485° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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