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 64728U 26145.49965270 +.00000000 +00000-0 +36261-4 0 00002
2 64728 53.1586 184.1354 0001044 84.4851 275.6269 15.30200750 02
| Epoch (UTC): | 25 May 2026 11:59:29 |
| Eccentricity: | 0.0001044 |
| inclination: | 53.1586° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 184.1354° |
| argument of perigee: | 84.4851° |
| revolutions per day: | 15.30200750 |
| mean anomaly at epoch: | 275.6269° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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