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 64924U 26145.58267131 +.00000000 +00000-0 +61022-3 0 00003
2 64924 53.1585 347.9956 0001535 96.5003 263.6173 15.31722695 03
| Epoch (UTC): | 25 May 2026 13:59:02 |
| Eccentricity: | 0.0001535 |
| inclination: | 53.1585° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 347.9956° |
| argument of perigee: | 96.5003° |
| revolutions per day: | 15.31722695 |
| mean anomaly at epoch: | 263.6173° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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