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 45047U 26145.57885619 +.00000000 +00000-0 +91651-3 0 00005
2 45047 53.1572 279.2543 0002840 319.2456 40.8341 15.50439648 06
| Epoch (UTC): | 25 May 2026 13:53:33 |
| Eccentricity: | 0.0002840 |
| inclination: | 53.1572° |
| perigee height: | 414 km |
| apogee height: | 417 km |
| right ascension of ascending node: | 279.2543° |
| argument of perigee: | 319.2456° |
| revolutions per day: | 15.50439648 |
| mean anomaly at epoch: | 40.8341° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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