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 49156U 26145.18286770 +.00000000 +00000-0 +56095-4 0 00004
2 49156 70.0005 61.5831 0002938 267.5969 92.4853 14.98330871 04
| Epoch (UTC): | 25 May 2026 04:23:19 |
| Eccentricity: | 0.0002938 |
| inclination: | 70.0005° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 61.5831° |
| argument of perigee: | 267.5969° |
| revolutions per day: | 14.98330871 |
| mean anomaly at epoch: | 92.4853° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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