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 61516U 26145.28160594 +.00000000 +00000-0 +52151-5 0 00004
2 61516 53.1605 146.3530 0001360 71.7190 288.3959 15.31707439 02
| Epoch (UTC): | 25 May 2026 06:45:30 |
| Eccentricity: | 0.0001360 |
| inclination: | 53.1605° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 146.3530° |
| argument of perigee: | 71.7190° |
| revolutions per day: | 15.31707439 |
| mean anomaly at epoch: | 288.3959° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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