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 39490U 26145.56917535 +.00000000 +00000-0 +18492-3 0 00004
2 39490 82.4112 283.3123 0011926 326.0603 33.9858 15.02015579 07
| Epoch (UTC): | 25 May 2026 13:39:36 |
| Eccentricity: | 0.0011926 |
| inclination: | 82.4112° |
| perigee height: | 552 km |
| apogee height: | 569 km |
| right ascension of ascending node: | 283.3123° |
| argument of perigee: | 326.0603° |
| revolutions per day: | 15.02015579 |
| mean anomaly at epoch: | 33.9858° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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