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 64721U 26145.35062794 +.00000000 +00000-0 +21313-3 0 00000
2 64721 70.0002 121.1683 0003414 266.2263 93.8506 14.98336168 02
| Epoch (UTC): | 25 May 2026 08:24:54 |
| Eccentricity: | 0.0003414 |
| inclination: | 70.0002° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 121.1683° |
| argument of perigee: | 266.2263° |
| revolutions per day: | 14.98336168 |
| mean anomaly at epoch: | 93.8506° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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