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 40001U 26143.16823558 +.00000000 +00000-0 +00000-0 0 00002
2 40001 65.2477 314.5351 0006531 181.5135 178.4814 2.13105757 03
| Epoch (UTC): | 23 May 2026 04:02:15 |
| Eccentricity: | 0.0006531 |
| inclination: | 65.2477° |
| perigee height: | 19113 km |
| apogee height: | 19146 km |
| right ascension of ascending node: | 314.5351° |
| argument of perigee: | 181.5135° |
| revolutions per day: | 2.13105757 |
| mean anomaly at epoch: | 178.4814° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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