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 67242U 26145.51596233 +.00000000 +00000-0 +76252-4 0 00002
2 67242 50.0018 197.0796 0001000 248.1181 111.9585 13.29322684 02
| Epoch (UTC): | 25 May 2026 12:22:59 |
| Eccentricity: | 0.0001000 |
| inclination: | 50.0018° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 197.0796° |
| argument of perigee: | 248.1181° |
| revolutions per day: | 13.29322684 |
| mean anomaly at epoch: | 111.9585° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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