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 62470U 26145.01133400 +.00000000 +00000-0 +12876-2 0 00008
2 62470 43.0034 123.0281 0003478 271.2448 88.8021 15.70944007 06
| Epoch (UTC): | 25 May 2026 00:16:19 |
| Eccentricity: | 0.0003478 |
| inclination: | 43.0034° |
| perigee height: | 354 km |
| apogee height: | 359 km |
| right ascension of ascending node: | 123.0281° |
| argument of perigee: | 271.2448° |
| revolutions per day: | 15.70944007 |
| mean anomaly at epoch: | 88.8021° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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