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 62513U 26145.22678757 +.00000000 +00000-0 +19805-2 0 00007
2 62513 42.9992 329.5870 0001817 47.4343 312.6678 15.70924792 09
| Epoch (UTC): | 25 May 2026 05:26:34 |
| Eccentricity: | 0.0001817 |
| inclination: | 42.9992° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 329.5870° |
| argument of perigee: | 47.4343° |
| revolutions per day: | 15.70924792 |
| mean anomaly at epoch: | 312.6678° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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