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 53728U 26145.32546580 +.00000000 +00000-0 +47696-4 0 00005
2 53728 53.2134 270.0400 0001193 88.4083 271.7045 15.08834552 00
| Epoch (UTC): | 25 May 2026 07:48:40 |
| Eccentricity: | 0.0001193 |
| inclination: | 53.2134° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 270.0400° |
| argument of perigee: | 88.4083° |
| revolutions per day: | 15.08834552 |
| mean anomaly at epoch: | 271.7045° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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