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 65645U 26145.48160545 +.00000000 +00000-0 +63421-3 0 00009
2 65645 53.1604 310.7157 0001152 100.8991 259.2139 15.30208772 04
| Epoch (UTC): | 25 May 2026 11:33:30 |
| Eccentricity: | 0.0001152 |
| inclination: | 53.1604° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 310.7157° |
| argument of perigee: | 100.8991° |
| revolutions per day: | 15.30208772 |
| mean anomaly at epoch: | 259.2139° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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