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 64104U 26145.39919083 +.00000000 +00000-0 +67026-3 0 00002
2 64104 53.1616 30.6985 0001206 86.2776 273.8363 15.30217552 08
| Epoch (UTC): | 25 May 2026 09:34:50 |
| Eccentricity: | 0.0001206 |
| inclination: | 53.1616° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 30.6985° |
| argument of perigee: | 86.2776° |
| revolutions per day: | 15.30217552 |
| mean anomaly at epoch: | 273.8363° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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