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 61016U 26145.48736559 +.00000000 +00000-0 +18244-3 0 00004
2 61016 49.9968 188.6338 0016854 349.1208 10.9364 14.84151594 04
| Epoch (UTC): | 25 May 2026 11:41:48 |
| Eccentricity: | 0.0016854 |
| inclination: | 49.9968° |
| perigee height: | 604 km |
| apogee height: | 628 km |
| right ascension of ascending node: | 188.6338° |
| argument of perigee: | 349.1208° |
| revolutions per day: | 14.84151594 |
| mean anomaly at epoch: | 10.9364° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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