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 49146U 26145.22054796 +.00000000 +00000-0 +23155-4 0 00000
2 49146 70.0003 82.5328 0002857 268.4774 91.6057 14.97523048 05
| Epoch (UTC): | 25 May 2026 05:17:35 |
| Eccentricity: | 0.0002857 |
| inclination: | 70.0003° |
| perigee height: | 573 km |
| apogee height: | 577 km |
| right ascension of ascending node: | 82.5328° |
| argument of perigee: | 268.4774° |
| revolutions per day: | 14.97523048 |
| mean anomaly at epoch: | 91.6057° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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