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 26071.94721139 +.00000000 +00000-0 +26591-3 0 00003
2 52898 98.2041 216.5432 0007263 335.1875 24.8977 14.63504836 08
| Epoch (UTC): | 12 March 2026 22:43:59 |
| Eccentricity: | 0.0007263 |
| inclination: | 98.2041° |
| perigee height: | 677 km |
| apogee height: | 687 km |
| right ascension of ascending node: | 216.5432° |
| argument of perigee: | 335.1875° |
| revolutions per day: | 14.63504836 |
| mean anomaly at epoch: | 24.8977° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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