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 62040U 26145.48665625 +.00000000 +00000-0 +32695-3 0 00003
2 62040 43.0016 190.1457 0001880 276.2317 83.8320 15.27571839 02
| Epoch (UTC): | 25 May 2026 11:40:47 |
| Eccentricity: | 0.0001880 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 190.1457° |
| argument of perigee: | 276.2317° |
| revolutions per day: | 15.27571839 |
| mean anomaly at epoch: | 83.8320° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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