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 47649U 26145.43171719 +.00000000 +00000-0 +75785-3 0 00009
2 47649 53.0362 352.6100 0002882 311.6721 48.4053 15.81588683 06
| Epoch (UTC): | 25 May 2026 10:21:40 |
| Eccentricity: | 0.0002882 |
| inclination: | 53.0362° |
| perigee height: | 324 km |
| apogee height: | 328 km |
| right ascension of ascending node: | 352.6100° |
| argument of perigee: | 311.6721° |
| revolutions per day: | 15.81588683 |
| mean anomaly at epoch: | 48.4053° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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