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 60039U 26145.57895959 +.00000000 +00000-0 +26123-4 0 00004
2 60039 53.1570 247.5052 0001168 97.8677 262.2473 15.69706115 03
| Epoch (UTC): | 25 May 2026 13:53:42 |
| Eccentricity: | 0.0001168 |
| inclination: | 53.1570° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 247.5052° |
| argument of perigee: | 97.8677° |
| revolutions per day: | 15.69706115 |
| mean anomaly at epoch: | 262.2473° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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