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 45360U 26145.12095983 +.00000000 +00000-0 +52530-3 0 00004
2 45360 53.0357 83.3079 0008780 65.8479 294.3456 15.72382251 04
| Epoch (UTC): | 25 May 2026 02:54:10 |
| Eccentricity: | 0.0008780 |
| inclination: | 53.0357° |
| perigee height: | 346 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 83.3079° |
| argument of perigee: | 65.8479° |
| revolutions per day: | 15.72382251 |
| mean anomaly at epoch: | 294.3456° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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