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 66262U 26145.40936700 +.00000000 +00000-0 +61924-3 0 00007
2 66262 53.1586 287.4555 0001090 90.4001 269.7125 15.30216118 02
| Epoch (UTC): | 25 May 2026 09:49:29 |
| Eccentricity: | 0.0001090 |
| inclination: | 53.1586° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 287.4555° |
| argument of perigee: | 90.4001° |
| revolutions per day: | 15.30216118 |
| mean anomaly at epoch: | 269.7125° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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