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 67221U 26145.45488279 +.00000000 +00000-0 +43394-3 0 00002
2 67221 45.0023 204.1922 0004006 23.4163 336.6895 15.08729543 07
| Epoch (UTC): | 25 May 2026 10:55:01 |
| Eccentricity: | 0.0004006 |
| inclination: | 45.0023° |
| perigee height: | 537 km |
| apogee height: | 543 km |
| right ascension of ascending node: | 204.1922° |
| argument of perigee: | 23.4163° |
| revolutions per day: | 15.08729543 |
| mean anomaly at epoch: | 336.6895° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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