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 57401U 26145.61293725 +.00000000 +00000-0 +22047-3 0 00001
2 57401 97.2556 196.0043 0002564 184.9765 175.1450 15.29528893 08
| Epoch (UTC): | 25 May 2026 14:42:37 |
| Eccentricity: | 0.0002564 |
| inclination: | 97.2556° |
| perigee height: | 475 km |
| apogee height: | 479 km |
| right ascension of ascending node: | 196.0043° |
| argument of perigee: | 184.9765° |
| revolutions per day: | 15.29528893 |
| mean anomaly at epoch: | 175.1450° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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