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 61871U 26145.60377112 +.00000000 +00000-0 +43654-3 0 00006
2 61871 97.4250 215.0179 0013277 71.0706 289.1970 15.24950957 01
| Epoch (UTC): | 25 May 2026 14:29:25 |
| Eccentricity: | 0.0013277 |
| inclination: | 97.4250° |
| perigee height: | 482 km |
| apogee height: | 500 km |
| right ascension of ascending node: | 215.0179° |
| argument of perigee: | 71.0706° |
| revolutions per day: | 15.24950957 |
| mean anomaly at epoch: | 289.1970° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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