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 53638U 26145.54899006 +.00000000 +00000-0 -11003-3 0 00006
2 53638 53.2105 238.7185 0001617 88.7070 271.4108 15.08836328 09
| Epoch (UTC): | 25 May 2026 13:10:32 |
| Eccentricity: | 0.0001617 |
| inclination: | 53.2105° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 238.7185° |
| argument of perigee: | 88.7070° |
| revolutions per day: | 15.08836328 |
| mean anomaly at epoch: | 271.4108° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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