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 64712U 26145.32558209 +.00000000 +00000-0 +27928-3 0 00006
2 64712 70.0001 121.0614 0003416 268.6406 91.4362 14.98336611 08
| Epoch (UTC): | 25 May 2026 07:48:50 |
| Eccentricity: | 0.0003416 |
| inclination: | 70.0001° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 121.0614° |
| argument of perigee: | 268.6406° |
| revolutions per day: | 14.98336611 |
| mean anomaly at epoch: | 91.4362° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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