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 39473U 26145.46925640 +.00000000 +00000-0 +99660-3 0 00006
2 39473 120.4648 41.4955 0072303 30.9601 329.5727 15.58695324 08
| Epoch (UTC): | 25 May 2026 11:15:43 |
| Eccentricity: | 0.0072303 |
| inclination: | 120.4648° |
| perigee height: | 342 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 41.4955° |
| argument of perigee: | 30.9601° |
| revolutions per day: | 15.58695324 |
| mean anomaly at epoch: | 329.5727° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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