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 49135U 26145.46242124 +.00000000 +00000-0 -12431-3 0 00003
2 49135 70.0003 60.8660 0002879 274.4225 85.6605 14.98341482 06
| Epoch (UTC): | 25 May 2026 11:05:53 |
| Eccentricity: | 0.0002879 |
| inclination: | 70.0003° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 60.8660° |
| argument of perigee: | 274.4225° |
| revolutions per day: | 14.98341482 |
| mean anomaly at epoch: | 85.6605° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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