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 57197U 26145.47835690 +.00000000 +00000-0 +51643-3 0 00004
2 57197 97.5092 214.5892 0008451 152.0137 208.1563 15.36044445 02
| Epoch (UTC): | 25 May 2026 11:28:50 |
| Eccentricity: | 0.0008451 |
| inclination: | 97.5092° |
| perigee height: | 452 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 214.5892° |
| argument of perigee: | 152.0137° |
| revolutions per day: | 15.36044445 |
| mean anomaly at epoch: | 208.1563° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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