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 45408U 26145.21438338 +.00000000 +00000-0 +75670-3 0 00002
2 45408 53.0393 116.1573 0007710 33.8003 326.3502 15.67457441 07
| Epoch (UTC): | 25 May 2026 05:08:42 |
| Eccentricity: | 0.0007710 |
| inclination: | 53.0393° |
| perigee height: | 361 km |
| apogee height: | 371 km |
| right ascension of ascending node: | 116.1573° |
| argument of perigee: | 33.8003° |
| revolutions per day: | 15.67457441 |
| mean anomaly at epoch: | 326.3502° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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