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 61885U 26145.51277154 +.00000000 +00000-0 +87201-5 0 00004
2 61885 53.1592 337.3239 0000912 86.0827 274.0295 15.69709053 02
| Epoch (UTC): | 25 May 2026 12:18:23 |
| Eccentricity: | 0.0000912 |
| inclination: | 53.1592° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 337.3239° |
| argument of perigee: | 86.0827° |
| revolutions per day: | 15.69709053 |
| mean anomaly at epoch: | 274.0295° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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