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 49179U 26145.48746175 +.00000000 +00000-0 -77501-5 0 00009
2 49179 70.0008 60.8136 0002544 269.8921 90.1946 14.98328949 09
| Epoch (UTC): | 25 May 2026 11:41:56 |
| Eccentricity: | 0.0002544 |
| inclination: | 70.0008° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 60.8136° |
| argument of perigee: | 269.8921° |
| revolutions per day: | 14.98328949 |
| mean anomaly at epoch: | 90.1946° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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