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 67442U 26145.34300836 +.00000000 +00000-0 +88629-4 0 00008
2 67442 50.0070 167.4981 0000843 286.0018 74.0761 13.29328256 09
| Epoch (UTC): | 25 May 2026 08:13:55 |
| Eccentricity: | 0.0000843 |
| inclination: | 50.0070° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 167.4981° |
| argument of perigee: | 286.0018° |
| revolutions per day: | 13.29328256 |
| mean anomaly at epoch: | 74.0761° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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