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 61632U 26145.52286486 +.00000000 +00000-0 +32901-4 0 00009
2 61632 43.0006 84.3485 0000792 263.5506 96.5255 15.27569648 05
| Epoch (UTC): | 25 May 2026 12:32:55 |
| Eccentricity: | 0.0000792 |
| inclination: | 43.0006° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 84.3485° |
| argument of perigee: | 263.5506° |
| revolutions per day: | 15.27569648 |
| mean anomaly at epoch: | 96.5255° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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