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 61628U 26145.50920971 +.00000000 +00000-0 -42659-4 0 00008
2 61628 42.9992 80.7783 0000762 260.5777 99.4988 15.27581624 00
| Epoch (UTC): | 25 May 2026 12:13:15 |
| Eccentricity: | 0.0000762 |
| inclination: | 42.9992° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 80.7783° |
| argument of perigee: | 260.5777° |
| revolutions per day: | 15.27581624 |
| mean anomaly at epoch: | 99.4988° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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