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 62987U 26145.31211882 +.00000000 +00000-0 +20090-2 0 00002
2 62987 42.9996 259.5571 0006929 289.4272 70.5847 15.71012469 04
| Epoch (UTC): | 25 May 2026 07:29:27 |
| Eccentricity: | 0.0006929 |
| inclination: | 42.9996° |
| perigee height: | 351 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 259.5571° |
| argument of perigee: | 289.4272° |
| revolutions per day: | 15.71012469 |
| mean anomaly at epoch: | 70.5847° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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