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 49755U 26145.44097044 +.00000000 +00000-0 -31731-4 0 00003
2 49755 53.2112 164.6198 0001163 85.8109 274.3016 15.08844127 06
| Epoch (UTC): | 25 May 2026 10:34:59 |
| Eccentricity: | 0.0001163 |
| inclination: | 53.2112° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 164.6198° |
| argument of perigee: | 85.8109° |
| revolutions per day: | 15.08844127 |
| mean anomaly at epoch: | 274.3016° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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