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 53849U 26145.46160916 +.00000000 +00000-0 +15090-4 0 00002
2 53849 53.2146 309.3289 0001380 93.8331 266.2819 15.08838369 00
| Epoch (UTC): | 25 May 2026 11:04:43 |
| Eccentricity: | 0.0001380 |
| inclination: | 53.2146° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 309.3289° |
| argument of perigee: | 93.8331° |
| revolutions per day: | 15.08838369 |
| mean anomaly at epoch: | 266.2819° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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