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 45388U 26145.13890904 +.00000000 +00000-0 +51348-3 0 00007
2 45388 53.0370 104.1079 0005798 57.6943 302.4637 15.75496452 06
| Epoch (UTC): | 25 May 2026 03:20:01 |
| Eccentricity: | 0.0005798 |
| inclination: | 53.0370° |
| perigee height: | 339 km |
| apogee height: | 347 km |
| right ascension of ascending node: | 104.1079° |
| argument of perigee: | 57.6943° |
| revolutions per day: | 15.75496452 |
| mean anomaly at epoch: | 302.4637° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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