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 49454U 26145.51452507 +.00000000 +00000-0 +69177-4 0 00000
2 49454 53.2149 234.2389 0001113 86.2842 273.8277 15.08840713 02
| Epoch (UTC): | 25 May 2026 12:20:54 |
| Eccentricity: | 0.0001113 |
| inclination: | 53.2149° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 234.2389° |
| argument of perigee: | 86.2842° |
| revolutions per day: | 15.08840713 |
| mean anomaly at epoch: | 273.8277° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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