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 65472U 26145.33833933 +.00000000 +00000-0 +10839-2 0 00003
2 65472 53.1610 261.8290 0001212 104.9880 255.1257 15.34433982 05
| Epoch (UTC): | 25 May 2026 08:07:12 |
| Eccentricity: | 0.0001212 |
| inclination: | 53.1610° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 261.8290° |
| argument of perigee: | 104.9880° |
| revolutions per day: | 15.34433982 |
| mean anomaly at epoch: | 255.1257° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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