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 53967U 26145.54167347 +.00000000 +00000-0 +73349-5 0 00009
2 53967 53.2126 239.1540 0001109 90.2129 269.8991 15.08835849 04
| Epoch (UTC): | 25 May 2026 13:00:00 |
| Eccentricity: | 0.0001109 |
| inclination: | 53.2126° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 239.1540° |
| argument of perigee: | 90.2129° |
| revolutions per day: | 15.08835849 |
| mean anomaly at epoch: | 269.8991° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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