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 49145U 26145.49163280 +.00000000 +00000-0 -11538-3 0 00009
2 49145 70.0010 60.7982 0003066 259.5880 100.4933 14.98333555 03
| Epoch (UTC): | 25 May 2026 11:47:57 |
| Eccentricity: | 0.0003066 |
| inclination: | 70.0010° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 60.7982° |
| argument of perigee: | 259.5880° |
| revolutions per day: | 14.98333555 |
| mean anomaly at epoch: | 100.4933° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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