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 52898U 26145.64591000 +.00000000 +00000-0 +14676-3 0 00005
2 52898 98.2184 289.9630 0009243 95.3851 264.8405 14.63645848 00
| Epoch (UTC): | 25 May 2026 15:30:06 |
| Eccentricity: | 0.0009243 |
| inclination: | 98.2184° |
| perigee height: | 675 km |
| apogee height: | 688 km |
| right ascension of ascending node: | 289.9630° |
| argument of perigee: | 95.3851° |
| revolutions per day: | 14.63645848 |
| mean anomaly at epoch: | 264.8405° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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