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 65486U 26143.60632594 +.00000000 +00000-0 +00000-0 0 00003
2 65486 28.7957 18.8473 0009888 173.7291 1.8552 1.00261227 05
| Epoch (UTC): | 23 May 2026 14:33:06 |
| Eccentricity: | 0.0009888 |
| inclination: | 28.7957° |
| perigee height: | 35748 km |
| apogee height: | 35831 km |
| right ascension of ascending node: | 18.8473° |
| argument of perigee: | 173.7291° |
| revolutions per day: | 1.00261227 |
| mean anomaly at epoch: | 1.8552° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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