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 53036U 26145.25371003 +.00000000 +00000-0 +36118-3 0 00001
2 53036 53.2132 90.4100 0001441 87.5853 272.5305 15.08859484 01
| Epoch (UTC): | 25 May 2026 06:05:20 |
| Eccentricity: | 0.0001441 |
| inclination: | 53.2132° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 90.4100° |
| argument of perigee: | 87.5853° |
| revolutions per day: | 15.08859484 |
| mean anomaly at epoch: | 272.5305° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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