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 62504U 26145.50002483 +.00000000 +00000-0 +72146-3 0 00003
2 62504 43.0017 214.7558 0001690 271.0790 88.9868 15.27587202 04
| Epoch (UTC): | 25 May 2026 12:00:02 |
| Eccentricity: | 0.0001690 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 214.7558° |
| argument of perigee: | 271.0790° |
| revolutions per day: | 15.27587202 |
| mean anomaly at epoch: | 88.9868° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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