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 62383U 26145.45847252 +.00000000 +00000-0 +25433-3 0 00000
2 62383 44.9940 56.0038 0001573 86.4675 273.6389 15.29472749 06
| Epoch (UTC): | 25 May 2026 11:00:12 |
| Eccentricity: | 0.0001573 |
| inclination: | 44.9940° |
| perigee height: | 476 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 56.0038° |
| argument of perigee: | 86.4675° |
| revolutions per day: | 15.29472749 |
| mean anomaly at epoch: | 273.6389° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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