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 61710U 26145.30399953 +.00000000 +00000-0 +33809-4 0 00004
2 61710 53.1603 105.6858 0001253 81.0666 279.0477 15.30198220 03
| Epoch (UTC): | 25 May 2026 07:17:45 |
| Eccentricity: | 0.0001253 |
| inclination: | 53.1603° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 105.6858° |
| argument of perigee: | 81.0666° |
| revolutions per day: | 15.30198220 |
| mean anomaly at epoch: | 279.0477° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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