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 40984U 26145.59369514 +.00000000 +00000-0 +00000-0 0 00008
2 40984 0.0390 109.4776 0002396 307.8371 89.5760 1.00270135 06
| Epoch (UTC): | 25 May 2026 14:14:55 |
| Eccentricity: | 0.0002396 |
| inclination: | 0.0390° |
| perigee height: | 35777 km |
| apogee height: | 35797 km |
| right ascension of ascending node: | 109.4776° |
| argument of perigee: | 307.8371° |
| revolutions per day: | 1.00270135 |
| mean anomaly at epoch: | 89.5760° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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