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 67441U 26145.42656196 +.00000000 +00000-0 +10065-3 0 00007
2 67441 50.0080 167.2829 0000743 278.8563 81.2225 13.29323932 02
| Epoch (UTC): | 25 May 2026 10:14:14 |
| Eccentricity: | 0.0000743 |
| inclination: | 50.0080° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 167.2829° |
| argument of perigee: | 278.8563° |
| revolutions per day: | 13.29323932 |
| mean anomaly at epoch: | 81.2225° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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