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 57213U 26145.15610237 +.00000000 +00000-0 +00000-0 0 00004
2 57213 0.0144 254.3907 0000654 181.7219 223.5176 1.00272263 02
| Epoch (UTC): | 25 May 2026 03:44:47 |
| Eccentricity: | 0.0000654 |
| inclination: | 0.0144° |
| perigee height: | 35784 km |
| apogee height: | 35789 km |
| right ascension of ascending node: | 254.3907° |
| argument of perigee: | 181.7219° |
| revolutions per day: | 1.00272263 |
| mean anomaly at epoch: | 223.5176° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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