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 40880U 26145.52883178 +.00000000 +00000-0 +00000-0 0 00003
2 40880 1.8615 82.8627 0003426 339.2342 93.8842 1.00273522 03
| Epoch (UTC): | 25 May 2026 12:41:31 |
| Eccentricity: | 0.0003426 |
| inclination: | 1.8615° |
| perigee height: | 35772 km |
| apogee height: | 35801 km |
| right ascension of ascending node: | 82.8627° |
| argument of perigee: | 339.2342° |
| revolutions per day: | 1.00273522 |
| mean anomaly at epoch: | 93.8842° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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