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 62620U 26145.20835909 +.00000000 +00000-0 +11829-2 0 00006
2 62620 97.3923 234.2535 0000918 23.5842 336.5456 15.57340422 02
| Epoch (UTC): | 25 May 2026 05:00:02 |
| Eccentricity: | 0.0000918 |
| inclination: | 97.3923° |
| perigee height: | 395 km |
| apogee height: | 396 km |
| right ascension of ascending node: | 234.2535° |
| argument of perigee: | 23.5842° |
| revolutions per day: | 15.57340422 |
| mean anomaly at epoch: | 336.5456° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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