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 65103U 26144.96951485 +.00000000 +00000-0 +39252-3 0 00006
2 65103 53.1589 31.9846 0000864 72.6057 287.5041 15.34402001 01
| Epoch (UTC): | 24 May 2026 23:16:06 |
| Eccentricity: | 0.0000864 |
| inclination: | 53.1589° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 31.9846° |
| argument of perigee: | 72.6057° |
| revolutions per day: | 15.34402001 |
| mean anomaly at epoch: | 287.5041° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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