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 53540U 26145.24458537 +.00000000 +00000-0 -50018-5 0 00006
2 53540 53.2159 80.8063 0001634 88.0421 272.0759 15.08834306 06
| Epoch (UTC): | 25 May 2026 05:52:12 |
| Eccentricity: | 0.0001634 |
| inclination: | 53.2159° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 80.8063° |
| argument of perigee: | 88.0421° |
| revolutions per day: | 15.08834306 |
| mean anomaly at epoch: | 272.0759° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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