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 57072U 26145.35746391 +.00000000 +00000-0 +20737-4 0 00003
2 57072 43.0033 23.3276 0000839 258.4588 101.6170 15.27577762 04
| Epoch (UTC): | 25 May 2026 08:34:44 |
| Eccentricity: | 0.0000839 |
| inclination: | 43.0033° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 23.3276° |
| argument of perigee: | 258.4588° |
| revolutions per day: | 15.27577762 |
| mean anomaly at epoch: | 101.6170° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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