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 53842U 26145.47266631 +.00000000 +00000-0 -25686-4 0 00000
2 53842 53.2122 309.3967 0001680 95.7391 264.3793 15.08836685 09
| Epoch (UTC): | 25 May 2026 11:20:38 |
| Eccentricity: | 0.0001680 |
| inclination: | 53.2122° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 309.3967° |
| argument of perigee: | 95.7391° |
| revolutions per day: | 15.08836685 |
| mean anomaly at epoch: | 264.3793° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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