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 61625U 26145.54889604 +.00000000 +00000-0 -10337-3 0 00003
2 61625 43.0047 80.2170 0001420 258.3659 101.7033 15.27588240 00
| Epoch (UTC): | 25 May 2026 13:10:24 |
| Eccentricity: | 0.0001420 |
| inclination: | 43.0047° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 80.2170° |
| argument of perigee: | 258.3659° |
| revolutions per day: | 15.27588240 |
| mean anomaly at epoch: | 101.7033° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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