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 64106U 26145.41288016 +.00000000 +00000-0 +73094-3 0 00004
2 64106 53.1616 30.0739 0000888 80.6633 279.4470 15.34408185 05
| Epoch (UTC): | 25 May 2026 09:54:32 |
| Eccentricity: | 0.0000888 |
| inclination: | 53.1616° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 30.0739° |
| argument of perigee: | 80.6633° |
| revolutions per day: | 15.34408185 |
| mean anomaly at epoch: | 279.4470° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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