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 27057U 26145.33059971 +.00000000 +00000-0 -24599-4 0 00003
2 27057 82.5453 228.7940 0001589 109.8998 250.2264 12.61616262 03
| Epoch (UTC): | 25 May 2026 07:56:03 |
| Eccentricity: | 0.0001589 |
| inclination: | 82.5453° |
| perigee height: | 1415 km |
| apogee height: | 1418 km |
| right ascension of ascending node: | 228.7940° |
| argument of perigee: | 109.8998° |
| revolutions per day: | 12.61616262 |
| mean anomaly at epoch: | 250.2264° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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