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 57503U 26145.44045228 +.00000000 +00000-0 -35263-3 0 00003
2 57503 43.0018 302.5685 0002461 256.2525 103.8053 15.27608716 00
| Epoch (UTC): | 25 May 2026 10:34:15 |
| Eccentricity: | 0.0002461 |
| inclination: | 43.0018° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 302.5685° |
| argument of perigee: | 256.2525° |
| revolutions per day: | 15.27608716 |
| mean anomaly at epoch: | 103.8053° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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