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 62100U 26145.40593175 +.00000000 +00000-0 +31665-3 0 00008
2 62100 42.9990 117.5812 0001369 270.1826 89.8868 15.27584717 08
| Epoch (UTC): | 25 May 2026 09:44:32 |
| Eccentricity: | 0.0001369 |
| inclination: | 42.9990° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 117.5812° |
| argument of perigee: | 270.1826° |
| revolutions per day: | 15.27584717 |
| mean anomaly at epoch: | 89.8868° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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