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 61610U 26145.39624551 +.00000000 +00000-0 +18445-2 0 00004
2 61610 87.8859 40.7953 0002045 112.9026 247.2317 13.10373647 02
| Epoch (UTC): | 25 May 2026 09:30:35 |
| Eccentricity: | 0.0002045 |
| inclination: | 87.8859° |
| perigee height: | 1220 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.7953° |
| argument of perigee: | 112.9026° |
| revolutions per day: | 13.10373647 |
| mean anomaly at epoch: | 247.2317° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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