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 53243U 26145.58027223 +.00000000 +00000-0 +22401-4 0 00000
2 53243 53.2121 218.6377 0000933 90.9358 269.1741 15.08837551 09
| Epoch (UTC): | 25 May 2026 13:55:35 |
| Eccentricity: | 0.0000933 |
| inclination: | 53.2121° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 218.6377° |
| argument of perigee: | 90.9358° |
| revolutions per day: | 15.08837551 |
| mean anomaly at epoch: | 269.1741° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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