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 51472U 26145.44371709 +.00000000 +00000-0 +12552-3 0 00003
2 51472 53.2142 294.4873 0001331 96.2229 263.8915 15.08848154 01
| Epoch (UTC): | 25 May 2026 10:38:57 |
| Eccentricity: | 0.0001331 |
| inclination: | 53.2142° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 294.4873° |
| argument of perigee: | 96.2229° |
| revolutions per day: | 15.08848154 |
| mean anomaly at epoch: | 263.8915° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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