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 53266U 26145.43402794 +.00000000 +00000-0 +49582-4 0 00008
2 53266 53.2113 209.6034 0001053 81.4162 278.6949 15.08839130 07
| Epoch (UTC): | 25 May 2026 10:25:00 |
| Eccentricity: | 0.0001053 |
| inclination: | 53.2113° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 209.6034° |
| argument of perigee: | 81.4162° |
| revolutions per day: | 15.08839130 |
| mean anomaly at epoch: | 278.6949° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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