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 64735U 26145.39541309 +.00000000 +00000-0 +31912-3 0 00009
2 64735 53.1579 184.9127 0001148 70.1206 289.9919 15.30206672 08
| Epoch (UTC): | 25 May 2026 09:29:23 |
| Eccentricity: | 0.0001148 |
| inclination: | 53.1579° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 184.9127° |
| argument of perigee: | 70.1206° |
| revolutions per day: | 15.30206672 |
| mean anomaly at epoch: | 289.9919° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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