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 57852U 26145.11439177 +.00000000 +00000-0 +44484-4 0 00009
2 57852 53.1613 288.8058 0001108 102.6936 257.4189 15.30196449 02
| Epoch (UTC): | 25 May 2026 02:44:43 |
| Eccentricity: | 0.0001108 |
| inclination: | 53.1613° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 288.8058° |
| argument of perigee: | 102.6936° |
| revolutions per day: | 15.30196449 |
| mean anomaly at epoch: | 257.4189° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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