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 52484U 26145.52924515 +.00000000 +00000-0 +19697-4 0 00003
2 52484 53.2139 74.1717 0001111 112.7762 247.3347 15.08844241 02
| Epoch (UTC): | 25 May 2026 12:42:06 |
| Eccentricity: | 0.0001111 |
| inclination: | 53.2139° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 74.1717° |
| argument of perigee: | 112.7762° |
| revolutions per day: | 15.08844241 |
| mean anomaly at epoch: | 247.3347° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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