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 49747U 26145.47313390 +.00000000 +00000-0 +77135-4 0 00009
2 49747 53.2109 164.4248 0001385 69.5030 290.6111 15.08832614 00
| Epoch (UTC): | 25 May 2026 11:21:18 |
| Eccentricity: | 0.0001385 |
| inclination: | 53.2109° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 164.4248° |
| argument of perigee: | 69.5030° |
| revolutions per day: | 15.08832614 |
| mean anomaly at epoch: | 290.6111° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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