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 62139U 26144.90491323 +.00000000 +00000-0 +99929-3 0 00003
2 62139 43.0046 87.9201 0001626 258.0782 101.9887 15.27591417 00
| Epoch (UTC): | 24 May 2026 21:43:04 |
| Eccentricity: | 0.0001626 |
| inclination: | 43.0046° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 87.9201° |
| argument of perigee: | 258.0782° |
| revolutions per day: | 15.27591417 |
| mean anomaly at epoch: | 101.9887° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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