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 64739U 26145.39224462 +.00000000 +00000-0 +27746-3 0 00001
2 64739 53.1580 184.8859 0001110 76.7407 283.3717 15.30205496 06
| Epoch (UTC): | 25 May 2026 09:24:49 |
| Eccentricity: | 0.0001110 |
| inclination: | 53.1580° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 184.8859° |
| argument of perigee: | 76.7407° |
| revolutions per day: | 15.30205496 |
| mean anomaly at epoch: | 283.3717° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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