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 64738U 26145.48382911 +.00000000 +00000-0 -44552-4 0 00000
2 64738 53.1586 184.0403 0000900 68.9593 291.1504 15.30203846 01
| Epoch (UTC): | 25 May 2026 11:36:42 |
| Eccentricity: | 0.0000900 |
| inclination: | 53.1586° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 184.0403° |
| argument of perigee: | 68.9593° |
| revolutions per day: | 15.30203846 |
| mean anomaly at epoch: | 291.1504° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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