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 57855U 26145.11756375 +.00000000 +00000-0 +68911-5 0 00006
2 57855 53.1598 288.8241 0001177 102.4581 257.6552 15.30188159 06
| Epoch (UTC): | 25 May 2026 02:49:17 |
| Eccentricity: | 0.0001177 |
| inclination: | 53.1598° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 288.8241° |
| argument of perigee: | 102.4581° |
| revolutions per day: | 15.30188159 |
| mean anomaly at epoch: | 257.6552° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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