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 60042U 26145.56425036 +.00000000 +00000-0 -58674-5 0 00000
2 60042 53.1576 247.4021 0000720 294.8760 65.2183 15.69693658 09
| Epoch (UTC): | 25 May 2026 13:32:31 |
| Eccentricity: | 0.0000720 |
| inclination: | 53.1576° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 247.4021° |
| argument of perigee: | 294.8760° |
| revolutions per day: | 15.69693658 |
| mean anomaly at epoch: | 65.2183° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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