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 62471U 26145.62594843 +.00000000 +00000-0 +19405-2 0 00003
2 62471 42.9999 119.0240 0002405 60.2239 299.8867 15.70898591 06
| Epoch (UTC): | 25 May 2026 15:01:21 |
| Eccentricity: | 0.0002405 |
| inclination: | 42.9999° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 119.0240° |
| argument of perigee: | 60.2239° |
| revolutions per day: | 15.70898591 |
| mean anomaly at epoch: | 299.8867° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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