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 53005U 26145.10098902 +.00000000 +00000-0 +17977-4 0 00008
2 53005 53.2150 111.0980 0001419 77.2557 282.8594 15.08837897 03
| Epoch (UTC): | 25 May 2026 02:25:25 |
| Eccentricity: | 0.0001419 |
| inclination: | 53.2150° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 111.0980° |
| argument of perigee: | 77.2557° |
| revolutions per day: | 15.08837897 |
| mean anomaly at epoch: | 282.8594° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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