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 57241U 26145.48622988 +.00000000 +00000-0 +26293-4 0 00003
2 57241 43.0000 306.3078 0001537 250.6237 109.4448 15.27574004 01
| Epoch (UTC): | 25 May 2026 11:40:10 |
| Eccentricity: | 0.0001537 |
| inclination: | 43.0000° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 306.3078° |
| argument of perigee: | 250.6237° |
| revolutions per day: | 15.27574004 |
| mean anomaly at epoch: | 109.4448° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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