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 57199U 26145.47988192 +.00000000 +00000-0 +52615-3 0 00002
2 57199 97.5092 215.4947 0007957 146.5625 213.6123 15.37617201 05
| Epoch (UTC): | 25 May 2026 11:31:01 |
| Eccentricity: | 0.0007957 |
| inclination: | 97.5092° |
| perigee height: | 448 km |
| apogee height: | 459 km |
| right ascension of ascending node: | 215.4947° |
| argument of perigee: | 146.5625° |
| revolutions per day: | 15.37617201 |
| mean anomaly at epoch: | 213.6123° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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