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 60242U 26144.76416050 +.00000000 +00000-0 +47373-3 0 00000
2 60242 61.9791 288.7115 0043477 125.9418 234.5723 15.12086397 04
| Epoch (UTC): | 24 May 2026 18:20:23 |
| Eccentricity: | 0.0043477 |
| inclination: | 61.9791° |
| perigee height: | 500 km |
| apogee height: | 560 km |
| right ascension of ascending node: | 288.7115° |
| argument of perigee: | 125.9418° |
| revolutions per day: | 15.12086397 |
| mean anomaly at epoch: | 234.5723° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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