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 67550U 26145.26083737 +.00000000 +00000-0 +72401-3 0 00007
2 67550 97.2861 32.3854 0001241 124.8301 235.3058 15.33460460 08
| Epoch (UTC): | 25 May 2026 06:15:36 |
| Eccentricity: | 0.0001241 |
| inclination: | 97.2861° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 32.3854° |
| argument of perigee: | 124.8301° |
| revolutions per day: | 15.33460460 |
| mean anomaly at epoch: | 235.3058° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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