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 57231U 26145.51947900 +.00000000 +00000-0 +20333-5 0 00000
2 57231 43.0032 316.9891 0001110 274.2707 85.8018 15.27572935 07
| Epoch (UTC): | 25 May 2026 12:28:02 |
| Eccentricity: | 0.0001110 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 316.9891° |
| argument of perigee: | 274.2707° |
| revolutions per day: | 15.27572935 |
| mean anomaly at epoch: | 85.8018° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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