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 39469U 26145.14895933 +.00000000 +00000-0 +35928-3 0 00004
2 39469 120.4893 263.1710 0141909 354.2785 5.6668 15.17682606 01
| Epoch (UTC): | 25 May 2026 03:34:30 |
| Eccentricity: | 0.0141909 |
| inclination: | 120.4893° |
| perigee height: | 415 km |
| apogee height: | 611 km |
| right ascension of ascending node: | 263.1710° |
| argument of perigee: | 354.2785° |
| revolutions per day: | 15.17682606 |
| mean anomaly at epoch: | 5.6668° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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