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 61884U 26145.52257748 +.00000000 +00000-0 +12749-4 0 00005
2 61884 53.1582 337.3883 0000581 110.1443 249.9638 15.69713041 04
| Epoch (UTC): | 25 May 2026 12:32:30 |
| Eccentricity: | 0.0000581 |
| inclination: | 53.1582° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 337.3883° |
| argument of perigee: | 110.1443° |
| revolutions per day: | 15.69713041 |
| mean anomaly at epoch: | 249.9638° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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