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 53289U 26145.53294382 +.00000000 +00000-0 -26849-4 0 00008
2 53289 53.2125 194.3000 0001010 93.7682 266.3425 15.08841533 07
| Epoch (UTC): | 25 May 2026 12:47:26 |
| Eccentricity: | 0.0001010 |
| inclination: | 53.2125° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 194.3000° |
| argument of perigee: | 93.7682° |
| revolutions per day: | 15.08841533 |
| mean anomaly at epoch: | 266.3425° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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