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 49455U 26145.63228416 +.00000000 +00000-0 +44693-4 0 00000
2 49455 53.2127 233.7093 0000862 84.3861 275.7229 15.08843441 04
| Epoch (UTC): | 25 May 2026 15:10:29 |
| Eccentricity: | 0.0000862 |
| inclination: | 53.2127° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 233.7093° |
| argument of perigee: | 84.3861° |
| revolutions per day: | 15.08843441 |
| mean anomaly at epoch: | 275.7229° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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