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 51998U 26145.40413720 +.00000000 +00000-0 +21558-3 0 00008
2 51998 53.2130 34.7333 0001280 84.9255 275.1883 15.08819443 02
| Epoch (UTC): | 25 May 2026 09:41:57 |
| Eccentricity: | 0.0001280 |
| inclination: | 53.2130° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 34.7333° |
| argument of perigee: | 84.9255° |
| revolutions per day: | 15.08819443 |
| mean anomaly at epoch: | 275.1883° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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