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 55633U 26145.02998713 +.00000000 +00000-0 -31476-3 0 00007
2 55633 69.9997 11.9607 0002967 263.5393 96.5428 14.98341766 05
| Epoch (UTC): | 25 May 2026 00:43:10 |
| Eccentricity: | 0.0002967 |
| inclination: | 69.9997° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 11.9607° |
| argument of perigee: | 263.5393° |
| revolutions per day: | 14.98341766 |
| mean anomaly at epoch: | 96.5428° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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