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 55747U 26145.09722095 +.00000000 +00000-0 +10201-3 0 00000
2 55747 70.0006 51.8730 0002715 264.3372 95.7477 14.98334784 09
| Epoch (UTC): | 25 May 2026 02:19:59 |
| Eccentricity: | 0.0002715 |
| inclination: | 70.0006° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 51.8730° |
| argument of perigee: | 264.3372° |
| revolutions per day: | 14.98334784 |
| mean anomaly at epoch: | 95.7477° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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