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 57860U 26145.12063685 +.00000000 +00000-0 +41489-4 0 00008
2 57860 53.1617 288.8408 0001223 105.4966 254.6170 15.31701064 01
| Epoch (UTC): | 25 May 2026 02:53:43 |
| Eccentricity: | 0.0001223 |
| inclination: | 53.1617° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 288.8408° |
| argument of perigee: | 105.4966° |
| revolutions per day: | 15.31701064 |
| mean anomaly at epoch: | 254.6170° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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