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 62473U 26145.33457769 +.00000000 +00000-0 +13561-2 0 00005
2 62473 43.0014 121.1550 0002430 287.5909 72.4693 15.70988670 02
| Epoch (UTC): | 25 May 2026 08:01:47 |
| Eccentricity: | 0.0002430 |
| inclination: | 43.0014° |
| perigee height: | 354 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 121.1550° |
| argument of perigee: | 287.5909° |
| revolutions per day: | 15.70988670 |
| mean anomaly at epoch: | 72.4693° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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