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 60040U 26144.68268345 +.00000000 +00000-0 +73205-5 0 00004
2 60040 53.1614 251.8647 0000582 91.2004 268.9081 15.69712017 09
| Epoch (UTC): | 24 May 2026 16:23:03 |
| Eccentricity: | 0.0000582 |
| inclination: | 53.1614° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 251.8647° |
| argument of perigee: | 91.2004° |
| revolutions per day: | 15.69712017 |
| mean anomaly at epoch: | 268.9081° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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