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 62589U 26145.05354277 +.00000000 +00000-0 +10323-2 0 00005
2 62589 43.0016 25.9285 0001765 266.3535 93.7131 15.70840113 00
| Epoch (UTC): | 25 May 2026 01:17:06 |
| Eccentricity: | 0.0001765 |
| inclination: | 43.0016° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 25.9285° |
| argument of perigee: | 266.3535° |
| revolutions per day: | 15.70840113 |
| mean anomaly at epoch: | 93.7131° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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