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 53790U 26145.36778181 +.00000000 +00000-0 +11425-3 0 00002
2 53790 53.2124 289.7758 0001305 97.7015 262.4125 15.08838417 04
| Epoch (UTC): | 25 May 2026 08:49:36 |
| Eccentricity: | 0.0001305 |
| inclination: | 53.2124° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 289.7758° |
| argument of perigee: | 97.7015° |
| revolutions per day: | 15.08838417 |
| mean anomaly at epoch: | 262.4125° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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