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 49147U 26145.17032772 +.00000000 +00000-0 +23524-3 0 00004
2 49147 70.0004 61.6258 0002866 267.1053 92.9778 14.98356474 05
| Epoch (UTC): | 25 May 2026 04:05:16 |
| Eccentricity: | 0.0002866 |
| inclination: | 70.0004° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 61.6258° |
| argument of perigee: | 267.1053° |
| revolutions per day: | 14.98356474 |
| mean anomaly at epoch: | 92.9778° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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