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 45390U 26145.11567626 +.00000000 +00000-0 +43358-3 0 00002
2 45390 53.0402 118.7505 0005192 6.6310 353.4773 15.68101068 05
| Epoch (UTC): | 25 May 2026 02:46:34 |
| Eccentricity: | 0.0005192 |
| inclination: | 53.0402° |
| perigee height: | 361 km |
| apogee height: | 368 km |
| right ascension of ascending node: | 118.7505° |
| argument of perigee: | 6.6310° |
| revolutions per day: | 15.68101068 |
| mean anomaly at epoch: | 353.4773° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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