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 47362U 26145.07433632 +.00000000 +00000-0 +11699-2 0 00009
2 47362 53.1587 66.9943 0001725 111.7254 248.3932 15.33979082 04
| Epoch (UTC): | 25 May 2026 01:47:02 |
| Eccentricity: | 0.0001725 |
| inclination: | 53.1587° |
| perigee height: | 463 km |
| apogee height: | 465 km |
| right ascension of ascending node: | 66.9943° |
| argument of perigee: | 111.7254° |
| revolutions per day: | 15.33979082 |
| mean anomaly at epoch: | 248.3932° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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