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 49151U 26145.21624760 +.00000000 +00000-0 +30909-4 0 00004
2 49151 70.0009 61.4997 0002779 270.6519 89.4322 14.98330777 06
| Epoch (UTC): | 25 May 2026 05:11:23 |
| Eccentricity: | 0.0002779 |
| inclination: | 70.0009° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 61.4997° |
| argument of perigee: | 270.6519° |
| revolutions per day: | 14.98330777 |
| mean anomaly at epoch: | 89.4322° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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