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 64366U 26145.45151698 +.00000000 +00000-0 +15988-3 0 00009
2 64366 70.0006 200.7635 0003761 265.0934 94.9796 14.98338021 02
| Epoch (UTC): | 25 May 2026 10:50:11 |
| Eccentricity: | 0.0003761 |
| inclination: | 70.0006° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 200.7635° |
| argument of perigee: | 265.0934° |
| revolutions per day: | 14.98338021 |
| mean anomaly at epoch: | 94.9796° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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