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 62380U 26145.44226221 +.00000000 +00000-0 +28384-3 0 00001
2 62380 44.9960 54.2694 0003029 133.2659 226.8479 15.30484031 03
| Epoch (UTC): | 25 May 2026 10:36:51 |
| Eccentricity: | 0.0003029 |
| inclination: | 44.9960° |
| perigee height: | 472 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 54.2694° |
| argument of perigee: | 133.2659° |
| revolutions per day: | 15.30484031 |
| mean anomaly at epoch: | 226.8479° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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