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 57236U 26145.48237808 +.00000000 +00000-0 -99191-6 0 00000
2 57236 43.0029 306.2805 0001262 269.8910 90.1797 15.27571239 08
| Epoch (UTC): | 25 May 2026 11:34:37 |
| Eccentricity: | 0.0001262 |
| inclination: | 43.0029° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 306.2805° |
| argument of perigee: | 269.8910° |
| revolutions per day: | 15.27571239 |
| mean anomaly at epoch: | 90.1797° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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