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 61716U 26145.17970705 +.00000000 +00000-0 +32731-4 0 00008
2 61716 53.1609 106.3337 0001343 102.4187 257.6965 15.30201651 08
| Epoch (UTC): | 25 May 2026 04:18:46 |
| Eccentricity: | 0.0001343 |
| inclination: | 53.1609° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 106.3337° |
| argument of perigee: | 102.4187° |
| revolutions per day: | 15.30201651 |
| mean anomaly at epoch: | 257.6965° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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