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 57150U 26145.46580818 +.00000000 +00000-0 +95686-5 0 00008
2 57150 43.0009 196.7109 0001502 272.0128 88.0552 15.26762547 02
| Epoch (UTC): | 25 May 2026 11:10:45 |
| Eccentricity: | 0.0001502 |
| inclination: | 43.0009° |
| perigee height: | 484 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 196.7109° |
| argument of perigee: | 272.0128° |
| revolutions per day: | 15.26762547 |
| mean anomaly at epoch: | 88.0552° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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