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 45377U 26145.10537751 +.00000000 +00000-0 +44756-3 0 00005
2 45377 53.0378 119.5656 0001630 130.0832 230.0328 15.69533030 07
| Epoch (UTC): | 25 May 2026 02:31:44 |
| Eccentricity: | 0.0001630 |
| inclination: | 53.0378° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 119.5656° |
| argument of perigee: | 130.0832° |
| revolutions per day: | 15.69533030 |
| mean anomaly at epoch: | 230.0328° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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