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 61627U 26145.52803882 +.00000000 +00000-0 +53606-3 0 00002
2 61627 43.0050 73.1318 0000549 291.9188 68.1605 15.27519993 02
| Epoch (UTC): | 25 May 2026 12:40:22 |
| Eccentricity: | 0.0000549 |
| inclination: | 43.0050° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 73.1318° |
| argument of perigee: | 291.9188° |
| revolutions per day: | 15.27519993 |
| mean anomaly at epoch: | 68.1605° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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