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 53251U 26145.34202904 +.00000000 +00000-0 +11976-4 0 00009
2 53251 53.2123 210.0132 0000977 69.2424 290.8673 15.08835808 04
| Epoch (UTC): | 25 May 2026 08:12:31 |
| Eccentricity: | 0.0000977 |
| inclination: | 53.2123° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 210.0132° |
| argument of perigee: | 69.2424° |
| revolutions per day: | 15.08835808 |
| mean anomaly at epoch: | 290.8673° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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